М.Г.Гоман, А.В.Храмцовский (1998) - Использование методов непрерывного продол...Project KRIT
М.Г.Гоман, А.В.Храмцовский "Использование методов непрерывного продолжения решений и бифуркационного анализа для синтеза систем управления", Phil.Trans.R.Soc.Lond. A (1998) 356, 2277-2295
M.G.Goman and A.V.Khramtsovsky "Application of continuation and bifurcation methods to the design of control systems", Phil.Trans.R.Soc.Lond. A (1998) 356, 2277-2295
In this paper the continuation and bifurcation methods are applied to aircraft nonlinear control design problems. The search for the recovery control from spin regimes is based on the minimization of an energy-like scalar function constrained by the aircraft's equilibria conditions. The design of a global stability augmentation system for severe wing-rock motion is performed by using bifurcation diagrams for equilibrium and periodical modes. The nonlinear control law, which totally suppresses wing-rock motion, is derived, taking into account both local stability characteristics of aircraft equilibrium states and domains of attraction, along with the requirement that all other attractors be eliminated.
Lid driven cavity flow simulation using CFD & MATLABIJSRD
Steady Incompressible Navier-Stokes equation on a uniform grid has been studied at various Reynolds number using CFD (Computational Fluid Dynamics). Present paper aim is to obtain the stream-function and velocity field in steady state using the finite difference formulation on momentum equations and continuity equation. Reynold number dominates the flow problem. Taylor’s series expansion has been used to convert the governing equations in the algebraic form using finite difference schemes. MATLAB has been used to draw to flow simulations inside the driven-cavity.
М.Г.Гоман, А.В.Храмцовский (1998) - Использование методов непрерывного продол...Project KRIT
М.Г.Гоман, А.В.Храмцовский "Использование методов непрерывного продолжения решений и бифуркационного анализа для синтеза систем управления", Phil.Trans.R.Soc.Lond. A (1998) 356, 2277-2295
M.G.Goman and A.V.Khramtsovsky "Application of continuation and bifurcation methods to the design of control systems", Phil.Trans.R.Soc.Lond. A (1998) 356, 2277-2295
In this paper the continuation and bifurcation methods are applied to aircraft nonlinear control design problems. The search for the recovery control from spin regimes is based on the minimization of an energy-like scalar function constrained by the aircraft's equilibria conditions. The design of a global stability augmentation system for severe wing-rock motion is performed by using bifurcation diagrams for equilibrium and periodical modes. The nonlinear control law, which totally suppresses wing-rock motion, is derived, taking into account both local stability characteristics of aircraft equilibrium states and domains of attraction, along with the requirement that all other attractors be eliminated.
Lid driven cavity flow simulation using CFD & MATLABIJSRD
Steady Incompressible Navier-Stokes equation on a uniform grid has been studied at various Reynolds number using CFD (Computational Fluid Dynamics). Present paper aim is to obtain the stream-function and velocity field in steady state using the finite difference formulation on momentum equations and continuity equation. Reynold number dominates the flow problem. Taylor’s series expansion has been used to convert the governing equations in the algebraic form using finite difference schemes. MATLAB has been used to draw to flow simulations inside the driven-cavity.
CFD and Artificial Neural Networks Analysis of Plane Sudden Expansion FlowsCSCJournals
It has been clearly established that the reattachment length for laminar flow depends on two non-dimensional parameters, the Reynolds number and the expansion ratio, therefore in this work, an ANN model that predict reattachment positions for the expansion ratios of 2, 3 and 5 based on the above two parameters has been developed. The R2 values of the testing set output Xr1, Xr2, Xr3, and Xr4 were 0.9383, 0.8577, 0.997 and 0.999 respectively. These results indicate that the network model produced reattachment positions that were in close agreement with the actual values. When considering the reattachment length of plane sudden-expansions the judicious combination of CFD calculated solutions with ANN will result in a considerable saving in computing and turnaround time. Thus CFD can be used in the first instance to obtain reattachment lengths for a limited choice of Reynolds numbers and ANN will be used subsequently to predict the reattachment lengths for other intermediate Reynolds number values. The CFD calculations concern unsteady laminar flow through a plane sudden expansion and are performed using a commercial CFD code STAR-CD while the training process of the corresponding ANN model was performed using the NeuroShellTM simulator.
This project aims at simulating lid driven cavity flow problem using package MATLAB. Steady Incompressible Navier-Stokes equation with continuity equation will be studied at various Reynolds number. The main aim is to obtain the velocity field in steady state using the finite difference formulation on momentum equations and continuity equation. Reynold number is the pertinent parameter of the present study. Taylor’s series expansion has been used to convert the governing equations in the algebraic form using finite difference schemes.
Using of intelligent communicational devices in controlling road structural w...IOSR Journals
The goal of this paper is to state and evaluate the differences in gap acceptance observations
between left lane and right lane change, and experiment overall aggressiveness by the means of right lane
change behaviors and use of electrical instruments for reaching this goal, furthermore we use Digital Signal
Processing on our controlling cameras to be able to distinguish different behaviours of drivers. Also, in this
paper we evaluate the decision making process of drivers, we do this work with use of electrical sensors for
accumulating some data and clarifying and processing them and finally with use of cumulative distribution
functions of driver lane change behaviours from the observed field data. These experiments are performed for
drivers using I-20 in Grand Prairie, Texas with the roadside controlling cameras and some other electronical
controlling instruments which were amounted near the intersection of I-20 and Great Southwest Blvd. Our
experiments and evaluations demonstrates, that the whole ratio of right lane change observations to left lane
change observations was close to 3 to 1.
A Novel Technique in Software Engineering for Building Scalable Large Paralle...Eswar Publications
Parallel processing is the only alternative for meeting computational demand of scientific and technological advancement. Yet first few parallelized versions of a large application code- in the present case-a meteorological Global Circulation Model- are not usually optimal or efficient. Large size and complexity of the code cause making changes for efficient parallelization and further validation difficult. The paper presents some novel techniques to enable change of parallelization strategy keeping the correctness of the code under control throughout the modification.
Aerodynamic Study about an Automotive Vehicle with Capacity for Only One Occu...IJERA Editor
The presented study describes the aerodynamic behavior of a compact, single occupant, automotive vehicle. To
optimize the aerodynamic characteristics of this vehicle, a flow dynamics study was conducted using a virtual
model. The outer surfaces of the vehicle body were designed using Computer Aided Design (CAD) tools and its
aerodynamic performance simulated virtually using Computational Fluid Dynamics (CFD) software. Parameters
such as pressure coefficient (Cp), coefficient of friction (Cf) and graphical analysis of the streamlines were used
to understand the flow dynamics and propose recommendations aimed at improving the coefficient of drag (Cd).
The identification of interaction points between the fluid and the flow structure was the primary focus of study to
develop these propositions. The study of phenomena linked to the characteristics of the model presented here,
allowed the identification of design features that should be avoided to generate improved aerodynamic
performance.
Choice of Numerical Integration Method for Wind Time History Analysis of Tall...inventy
Wind tunnel tests are being performed routinely around the world for designing tall buildings but the advent of powerful computational tools will make time-history analysis for wind more common in near future. As the duration of wind storms ranges from tens of minutes to hours while earthquake durations are typically less than a three to four minutes, the choice of a time step size (Δt) for wind studies needs to be much larger both to reduce the computational time and to save disk space. As the error in any numerical solution of the equation of motion is dependent on step size (Δt), careful investigations on the choice of numerical integration methods for wind analyses are necessary. From a wide variety of integration methods available, it was decided to investigate three methods that seem appropriate for 3D-time history analysis of tall buildings for wind. These are modal time history analysis, the Hilber-Hughes-Taylor (HHT) method or α-method with α=- 0.1, and the Newmark method with β=0.25 and γ=0.5 ( i.e., trapezoidal rule). SAP2000, a common structural analysis software tool, and a 64-story structure are used to conduct all the analyses in this paper. A boundary layer wind tunnel (BLWT) pressure time history measured at 120 locations around the building envelope of a similar structure is used for the analyses. Analyses performed with both the HHT and Newmark-method considering P-delta effects show that second order effects have a considerable impact on both displacement and acceleration response. This result shows that it is necessary to account P-delta effect for wind analysis of tall buildings. As the direct integration time history analysis required very large computation times and very large computer physical memory for a wind duration of hours, a modal analysis with reduced stiffness is considered as a good alternative. For that purpose, a non-linear static analysis of the structure with a load combination of 1.0D + 1.0L is performed in SAP2000 and the reduced stiffness of the structure after the analysis is used to conduct an eigenvalue analysis to extract the mode shapes and frequencies of this structure. Then the first 20- modes are used to perform a modal time history analysis for wind load. The result shows that the responses from modal analysis with “20-mode (reduced stiffness)” are comparable with that from the P-Δ analyses of Newmark-method
Review and Assessment of Turbulence Transition ModelsIJERDJOURNAL
ABSTRACT: Turbulent boundary layer transition can greatly affect flow characteristics such as skin friction, heat transfer, pressure loads, and boundary layer separation point. Accurate computation of such effect is vital to the design of components and vehicles subjected to turbulent transition flows. In this paper we report our review of the existing boundary layer transition models, selection of the boundary layer transition models most appropriate for the existing Reynolds-averaged Navier-Stokes flow solvers, and implementation and evaluation of the selected transition models with some benchmark test cases, ranging from subsonic to hypersonic flows. The objective of this assessment study is not intended to pick the best transition model (in fact, there is no transition model accurately predict the boundary layer transition for all cases tested here). Rather it is to demonstrate that (1) the flow physics of turbulence transition is very complicated and not yet well understood, (2) the applicability of empirical transition models is limited and their use should be cautious due to different transition characteristics for different flow regimes/environments, and (3) further research on prediction of turbulence transition is warranted to improve the accuracy, efficiency and range of applicability.
Review of Applicability of Prediction Model for Running Speed on Horizontal C...inventionjournals
In Korea's road design criteria, the guideline to evaluate the safety of horizontal curve and vertical curve is quantitatively suggested, but for a complex alignment where these two alignments are combined, qualitative guideline only is provided. Thus, the measure to quantitatively evaluate the safety of the complex alignment needs to be provided as early as possible. The useful approaches to the study introduced to date include the method to use running speed profile, the method to use the sight distance and the method to use the work load and the method to evaluate the safety of road alignment using running speed profile has been more widely applied than others. Many studies on evaluating the safety of road alignment using running speed profile have been conducted domestically which however are limited to the prediction model for running speed on horizontal alignment and the study on model to predict the complex alignment combining the horizontal alignment with vertical alignment has still been far behind. This study is intended to review the method using running speed profile among the methods to evaluate the safety of complex alignment and before developing the running speed prediction model considering the effect of complex alignment, the study was conducted as part of the review of the need for developing the model which is differentiated by the type of combination of horizontal alignment and vertical alignment. As part of the process, integrated running speed prediction model using the design elements of horizontal alignment as independent variable was developed which was then classified depending on combination pattern of horizontal alignment and vertical alignment and was compared with determination coefficient of prediction model for individual running speed. As a result, prediction model for individual running speed developed depending on combination pattern of horizontal alignment and vertical alignment was able to predict the running speed more accurately than integrated running speed prediction model, which implies the need for developing the running speed prediction model including the variables that incorporate the combination characteristics of unique horizontal alignment and vertical alignment.
1.Critically assess the aerodynamic characteristics of a vehicle.
2.Select and specify the most appropriate methods for wind tunnel testing of scale models and interpret the results of the test.
3.Analyse and critically evaluate the aerodynamic cooling systems.
SIMMECHANICS VISUALIZATION OF EXPERIMENTAL MODEL OVERHEAD CRANE, ITS LINEARIZ...ijccmsjournal
Overhead Crane experimental model using Simmechanic Visualization is presented for the robust antisway LQR control. First, 1D translational motion of overhead crane is designed with exact lab model measurements and features. Second, linear least square system identification with 7 past inputs/outputs is applied on collected simulation data to produce more predicted models. Third, minimize root mean square error and identified the best fit model with lowest RMSE. Finally, Linear Quadratic Regulator (LQR) and Reference tracking with pre-compensator have been implemented to minimize load swing and perform fast track on trolley positioning.
CFD and Artificial Neural Networks Analysis of Plane Sudden Expansion FlowsCSCJournals
It has been clearly established that the reattachment length for laminar flow depends on two non-dimensional parameters, the Reynolds number and the expansion ratio, therefore in this work, an ANN model that predict reattachment positions for the expansion ratios of 2, 3 and 5 based on the above two parameters has been developed. The R2 values of the testing set output Xr1, Xr2, Xr3, and Xr4 were 0.9383, 0.8577, 0.997 and 0.999 respectively. These results indicate that the network model produced reattachment positions that were in close agreement with the actual values. When considering the reattachment length of plane sudden-expansions the judicious combination of CFD calculated solutions with ANN will result in a considerable saving in computing and turnaround time. Thus CFD can be used in the first instance to obtain reattachment lengths for a limited choice of Reynolds numbers and ANN will be used subsequently to predict the reattachment lengths for other intermediate Reynolds number values. The CFD calculations concern unsteady laminar flow through a plane sudden expansion and are performed using a commercial CFD code STAR-CD while the training process of the corresponding ANN model was performed using the NeuroShellTM simulator.
This project aims at simulating lid driven cavity flow problem using package MATLAB. Steady Incompressible Navier-Stokes equation with continuity equation will be studied at various Reynolds number. The main aim is to obtain the velocity field in steady state using the finite difference formulation on momentum equations and continuity equation. Reynold number is the pertinent parameter of the present study. Taylor’s series expansion has been used to convert the governing equations in the algebraic form using finite difference schemes.
Using of intelligent communicational devices in controlling road structural w...IOSR Journals
The goal of this paper is to state and evaluate the differences in gap acceptance observations
between left lane and right lane change, and experiment overall aggressiveness by the means of right lane
change behaviors and use of electrical instruments for reaching this goal, furthermore we use Digital Signal
Processing on our controlling cameras to be able to distinguish different behaviours of drivers. Also, in this
paper we evaluate the decision making process of drivers, we do this work with use of electrical sensors for
accumulating some data and clarifying and processing them and finally with use of cumulative distribution
functions of driver lane change behaviours from the observed field data. These experiments are performed for
drivers using I-20 in Grand Prairie, Texas with the roadside controlling cameras and some other electronical
controlling instruments which were amounted near the intersection of I-20 and Great Southwest Blvd. Our
experiments and evaluations demonstrates, that the whole ratio of right lane change observations to left lane
change observations was close to 3 to 1.
A Novel Technique in Software Engineering for Building Scalable Large Paralle...Eswar Publications
Parallel processing is the only alternative for meeting computational demand of scientific and technological advancement. Yet first few parallelized versions of a large application code- in the present case-a meteorological Global Circulation Model- are not usually optimal or efficient. Large size and complexity of the code cause making changes for efficient parallelization and further validation difficult. The paper presents some novel techniques to enable change of parallelization strategy keeping the correctness of the code under control throughout the modification.
Aerodynamic Study about an Automotive Vehicle with Capacity for Only One Occu...IJERA Editor
The presented study describes the aerodynamic behavior of a compact, single occupant, automotive vehicle. To
optimize the aerodynamic characteristics of this vehicle, a flow dynamics study was conducted using a virtual
model. The outer surfaces of the vehicle body were designed using Computer Aided Design (CAD) tools and its
aerodynamic performance simulated virtually using Computational Fluid Dynamics (CFD) software. Parameters
such as pressure coefficient (Cp), coefficient of friction (Cf) and graphical analysis of the streamlines were used
to understand the flow dynamics and propose recommendations aimed at improving the coefficient of drag (Cd).
The identification of interaction points between the fluid and the flow structure was the primary focus of study to
develop these propositions. The study of phenomena linked to the characteristics of the model presented here,
allowed the identification of design features that should be avoided to generate improved aerodynamic
performance.
Choice of Numerical Integration Method for Wind Time History Analysis of Tall...inventy
Wind tunnel tests are being performed routinely around the world for designing tall buildings but the advent of powerful computational tools will make time-history analysis for wind more common in near future. As the duration of wind storms ranges from tens of minutes to hours while earthquake durations are typically less than a three to four minutes, the choice of a time step size (Δt) for wind studies needs to be much larger both to reduce the computational time and to save disk space. As the error in any numerical solution of the equation of motion is dependent on step size (Δt), careful investigations on the choice of numerical integration methods for wind analyses are necessary. From a wide variety of integration methods available, it was decided to investigate three methods that seem appropriate for 3D-time history analysis of tall buildings for wind. These are modal time history analysis, the Hilber-Hughes-Taylor (HHT) method or α-method with α=- 0.1, and the Newmark method with β=0.25 and γ=0.5 ( i.e., trapezoidal rule). SAP2000, a common structural analysis software tool, and a 64-story structure are used to conduct all the analyses in this paper. A boundary layer wind tunnel (BLWT) pressure time history measured at 120 locations around the building envelope of a similar structure is used for the analyses. Analyses performed with both the HHT and Newmark-method considering P-delta effects show that second order effects have a considerable impact on both displacement and acceleration response. This result shows that it is necessary to account P-delta effect for wind analysis of tall buildings. As the direct integration time history analysis required very large computation times and very large computer physical memory for a wind duration of hours, a modal analysis with reduced stiffness is considered as a good alternative. For that purpose, a non-linear static analysis of the structure with a load combination of 1.0D + 1.0L is performed in SAP2000 and the reduced stiffness of the structure after the analysis is used to conduct an eigenvalue analysis to extract the mode shapes and frequencies of this structure. Then the first 20- modes are used to perform a modal time history analysis for wind load. The result shows that the responses from modal analysis with “20-mode (reduced stiffness)” are comparable with that from the P-Δ analyses of Newmark-method
Review and Assessment of Turbulence Transition ModelsIJERDJOURNAL
ABSTRACT: Turbulent boundary layer transition can greatly affect flow characteristics such as skin friction, heat transfer, pressure loads, and boundary layer separation point. Accurate computation of such effect is vital to the design of components and vehicles subjected to turbulent transition flows. In this paper we report our review of the existing boundary layer transition models, selection of the boundary layer transition models most appropriate for the existing Reynolds-averaged Navier-Stokes flow solvers, and implementation and evaluation of the selected transition models with some benchmark test cases, ranging from subsonic to hypersonic flows. The objective of this assessment study is not intended to pick the best transition model (in fact, there is no transition model accurately predict the boundary layer transition for all cases tested here). Rather it is to demonstrate that (1) the flow physics of turbulence transition is very complicated and not yet well understood, (2) the applicability of empirical transition models is limited and their use should be cautious due to different transition characteristics for different flow regimes/environments, and (3) further research on prediction of turbulence transition is warranted to improve the accuracy, efficiency and range of applicability.
Review of Applicability of Prediction Model for Running Speed on Horizontal C...inventionjournals
In Korea's road design criteria, the guideline to evaluate the safety of horizontal curve and vertical curve is quantitatively suggested, but for a complex alignment where these two alignments are combined, qualitative guideline only is provided. Thus, the measure to quantitatively evaluate the safety of the complex alignment needs to be provided as early as possible. The useful approaches to the study introduced to date include the method to use running speed profile, the method to use the sight distance and the method to use the work load and the method to evaluate the safety of road alignment using running speed profile has been more widely applied than others. Many studies on evaluating the safety of road alignment using running speed profile have been conducted domestically which however are limited to the prediction model for running speed on horizontal alignment and the study on model to predict the complex alignment combining the horizontal alignment with vertical alignment has still been far behind. This study is intended to review the method using running speed profile among the methods to evaluate the safety of complex alignment and before developing the running speed prediction model considering the effect of complex alignment, the study was conducted as part of the review of the need for developing the model which is differentiated by the type of combination of horizontal alignment and vertical alignment. As part of the process, integrated running speed prediction model using the design elements of horizontal alignment as independent variable was developed which was then classified depending on combination pattern of horizontal alignment and vertical alignment and was compared with determination coefficient of prediction model for individual running speed. As a result, prediction model for individual running speed developed depending on combination pattern of horizontal alignment and vertical alignment was able to predict the running speed more accurately than integrated running speed prediction model, which implies the need for developing the running speed prediction model including the variables that incorporate the combination characteristics of unique horizontal alignment and vertical alignment.
1.Critically assess the aerodynamic characteristics of a vehicle.
2.Select and specify the most appropriate methods for wind tunnel testing of scale models and interpret the results of the test.
3.Analyse and critically evaluate the aerodynamic cooling systems.
SIMMECHANICS VISUALIZATION OF EXPERIMENTAL MODEL OVERHEAD CRANE, ITS LINEARIZ...ijccmsjournal
Overhead Crane experimental model using Simmechanic Visualization is presented for the robust antisway LQR control. First, 1D translational motion of overhead crane is designed with exact lab model measurements and features. Second, linear least square system identification with 7 past inputs/outputs is applied on collected simulation data to produce more predicted models. Third, minimize root mean square error and identified the best fit model with lowest RMSE. Finally, Linear Quadratic Regulator (LQR) and Reference tracking with pre-compensator have been implemented to minimize load swing and perform fast track on trolley positioning.
El uso de las Tic en educación es necesario porque nos encontramos en la era del conocimiento, existiendo un consenso en lo indispensable de las Tic para ayudar en los procesos de aprendizaje y de la enseñanza
Higher Education Options for Indian Students in the United StatesAnjana Krishnan
United States is one of the best destinations for higher education in the world. This article will clarify all the aspects of higher education in the US to the Indian students.
The need for high pump performance and efficiency continue to encourage the study of flow between two parallel co-rotating discs in multiple discs pump or turbine. Therefore, this study entails the design, construction and CFD simulation of a 3D Tesla pump model axisymmetric swirling flow in order to enhance the understanding of Tesla pump for future development.
Method of solution entails designing and construction of a small prototype tesla pump and then using the design geometry and parameters to design and perform numerical simulation. The results of the numerical simulation were then analyzed.
The result obtained indicates static pressure to have minimum value of -4.7791Pa at the outlet and 13.777Pa at the pump inlet and with velocity magnitude having minimum velocity of 0.00m/s and maximum velocity of 4.12m/s. The strength of the velocity was seen to be very high at the pump outlet. The analysis radial velocity showed minimum value of -0.508m/s and maximum value of 3.981m/s with the radial velocity vector being concentrated at the discs periphery and outlet.
Model simulation results exhibited smooth pressure and velocity profiles. With the 3D simulation all flow variables are able to be predicted.
The need for high pump performance and efficiency continue to encourage the study of flow between two parallel co-rotating discs in multiple discs pump or turbine. Therefore, this study entails the design, construction and CFD simulation of a 3D Tesla pump model axisymmetric swirling flow in order to enhance the understanding of Tesla pump for future development.
Method of solution entails designing and construction of a small prototype tesla pump and then using the design geometry and parameters to design and perform numerical simulation. The results of the numerical simulation were then analyzed.
The result obtained indicates static pressure to have minimum value of -4.7791Pa at the outlet and 13.777Pa at the pump inlet and with velocity magnitude having minimum velocity of 0.00m/s and maximum velocity of 4.12m/s. The strength of the velocity was seen to be very high at the pump outlet. The analysis radial velocity showed minimum value of -0.508m/s and maximum value of 3.981m/s with the radial velocity vector being concentrated at the discs periphery and outlet.
Model simulation results exhibited smooth pressure and velocity profiles. With the 3D simulation all flow variables are able to be predicted.
An Efficient Algorithm for Contact Angle Estimation in Molecular Dynamics Sim...CSCJournals
It is important to find contact angle for a liquid to understand its wetting properties, capillarity and surface interaction energy with a surface. The estimation of contact angle from Non Equilibrium Molecular Dynamics (NEMD), where we need to track the changes in contact angle over a period of time is challenging compared to the estimation from a single image from an experimental measurement. Often such molecular simulations involve finite number of molecules above some metallic or non-metallic substrates and coupled to a thermostat. The identification of profile of the droplet formed during this time will be difficult and computationally expensive to process as an image. In this paper a new algorithm is explained which can efficiently calculate time dependent contact angle from a NEMD simulation just by processing the molecular coordinates. The algorithm implements many simple yet accurate mathematical methods available, especially to remove the vapor molecules and noise data and thereby calculating the contact angle with more accuracy. To further demonstrate the capability of the algorithm a simulation study has been reported which compares the contact angle influence with different thermostats in the Molecular Dynamics (MD) simulation of water over platinum surface.
Comparison of Control Strategies of DSTATACOM for Non-linear Load Compensationidescitation
For load compensation a number of control strategies have been developed by
researchers but choice of control strategy is important to cope with the operating condition
of system. In this paper five control strategies viz. instantaneous p-q theory, synchronous
reference frame Method(SRF), Modified SRF Method(MSRF), instantaneous symmetrical
component theory(ISCT) and Average unit power factor theory(AUPFT) are compared for
different two conditions. The performance of the system simulated in Matlab Platform and
evaluated considering the source current total harmonic distortion. The result shows
Modified SRF(id-iq) Method has improved system performance as compared to others.
Aerodynamic Analysis of Low Speed Turbulent Flow Over A Delta WingIJRES Journal
Delta wing has been a subject of intense research since decades due to decades due to inherent characteristics of generating increased nonlinear lift due to vortex dominated flows. Lot of work has been carried out in order to understand the vortex dominated flows on the delta wing. The delta wing is a wing platform in the form of a triangle. Aerodynamics of wings with moderate sweep angle is recognized by the aerospace community as a challenging problem. In spite of its potential application in military aircraft, the understanding of the aerodynamics of such wings is far from complete. In order to address this situation, the present work is initiated to compute the 3D turbulent flow field over sharp edged finite wings with a diamond shaped plan forms and moderate sweep angle. The detailed flow pattern and surface pressure distribution may further indicate the appropriate kind of flow control during flight operation of such wings. The flow field is computed using an in-house developed CFD code RANS3D.
Synthesis of new antenna arrays with arbitrary geometries based on the super...IJECEIAES
The synthesis of antenna arrays with low sidelobe levels is needed to enhance the communication systems’ efficiency. In this paper, new arbitrary geometries that improve the ability of the antenna arrays to minimize the sidelobe level, are proposed. We employ the well-known superformula equation in the antenna arrays field by implementing the equation in the general array factor equation. Three metaheuristic optimization algorithms are used to synthesize the antenna arrays and their geometries; antlion optimization (ALO) algorithm, grasshopper optimization algorithm (GOA), and a new hybrid algorithm based on ALO and GOA. All the proposed algorithms are high-performance computational methods, which proved their efficiency for solving different real-world optimization problems. 15 design examples are presented and compared to prove validity with the most general standard geometry: elliptical antenna array (EAA). It is observed that the proposed geometries outperform EAA geometries by 4.5 dB and 10.9 dB in the worst and best scenarios, respectively, which proves the advantage and superiority of our approach.
Analysis of the Use of Universal Distribution Factors in SEC Power Gridresearchinventy
Distribution factors have been extensively used in many power system analysis and planning studies. In recent power system studies, the AC distribution factors are insensitive to the operating point and relatively sensitive at certain degree to changes in network topology. These factors are linear approximations of sensitivities of variables with various inputs. This paper presents the calculation of the universal distribution factors (UDF’s) applies them on several practical scenarios of Saudi Electricity Company (SEC) power grid. The results are analyzed and evaluated considering various system conditions of SEC load. The results show that the accuracy of the used approach is acceptable compared with exact method. This is practically beneficial to SEC in computing its grid complex power flows using UDF's at the base case without the need to recalculate UDF’s which save efforts and time.
The effect of rotational speed variation on the velocity vectors in the singl...IOSR Journals
The current investigation is aimed to simulate the three-dimensional complex internal flow in a
centrifugal pump impeller with five twisted blades by using a specialized computational fluid dynamics (CFD)
software ANSYS /FLUENT 14code with a standard k-ε two-equation turbulence model.
A single blade passage will be modeled to give more accurate results for velocity vectors on (blade, hub, and
shroud). The potential consequences of velocity vectors associated with operating a centrifugal compressor in
variable rotation speed.
A numerical three-dimensional, through flow calculations to predict velocity vectors through a
centrifugal pump were presented to examined the effect of rotational speed variation on the velocity vectors of
the centrifugal pump . The contours of the velocity vectors of the blade, hub, and shroud indicates low velocity
vectors in the suction side at high rotational speed (over operation limits )and the velocity vectors increases
gradually until reach maximum value at the leading edge (2.63×10 m/s) of the blade
Poster based on research on investigating the non-linear response of a synchronous machine to variations in system parameters (torque and damping), demonstrating the existence of a bifurcation curve within the parameter space. Response was visualized using state space diagrams. This poster was presented at the Power and Energy Conference at the University of Illinois (PECI) in Spring 2017.
A new lemma of the Optical Equivalence Theorem: applications in Theoretical C...Orchidea Maria Lecian
Talk delivered at 3rd Edition of Chemistry World Conference-
Chemistry2023.
14-15 June 2023.
Author: Orchidea Maria Lecian.
Speaker Orchidea Maria Lecian.
Title: A new lemma of the Optical Equivalence Theorem:
applications in Theoretical Chemistry and
new challenges.
Abstract: The Optical Equivalence Theorem demonstrates the equivalence between
the expectation value of an operator in the opportune Hilbert space and
the expectation value of the pertinent functional representation in the
phase space formulation with respect to a suitable distribution; for the
purposes of this demonstration, a phase space representation is chosen,
which does not involve the Number operator. The Optical Equivalence
Principle allows one to construct a sequence of the density operator.
A new lemma of the Optical Equivalence Theorem is demonstrated,
after which there is associated with the quasi-probability distribution and
improved functional representation as far as the allowed expansion order
is concerned; the construction is apt to codify almost-infinite-momentum
states. A compact-support control weighting function is introduced, to
display the action of operators of high-intensity fields, whose states are
determined.
Applications in Theoretical Chemistry are provided with. Applications are
explained within molecular dynamics trajectories: the atomic
coordinates at specific times are framed in the phase space, where the
new improved representation of the quasi-probability distribution is used
to improve the long-time-limit error calculation in the quantum
fluctuations, quantum jumps (also in lasing), comparison of chemical
shift with MNR spectroscopy for control of composition; Markovv
modelisation: the long-timescale dynamics of molecular systems is
analysed as consisting of probabilistic jumps between est of states, which
are now newly issued as those which are the pertinent states of the new
improved functional representation: quantum fluctuation, transition to
lasing, carrier energy states, comparison with Monte-Carlo simulation;
molecular chemistry: protein stability and folding kinetics, coordinate
shift with determination of transition states, transmission probability,
definition of entropic reaction coordinates; laser molecule activation;
transition-state spectroscopy: potential energy surfaces are newly
established within the new representation of the phase space; molecular
activation: the process of the molecular activation is framed within the
new representation of the states within the new representation of the
phase space obtained after the new improved representation of the
probability-distribution sequence. New challenges are envisaged
1. Improved analytical flux surface representation and calculation models for poloidal
asymmetries
T. G. Collart and W. M. Stacey
Citation: Physics of Plasmas 23, 052505 (2016); doi: 10.1063/1.4948552
View online: http://dx.doi.org/10.1063/1.4948552
View Table of Contents: http://scitation.aip.org/content/aip/journal/pop/23/5?ver=pdfcov
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2. Improved analytical flux surface representation and calculation models
for poloidal asymmetries
T. G. Collarta)
and W. M. Stacey
Georgia Institute of Technology, Atlanta, Georgia 30332, USA
(Received 18 January 2016; accepted 15 April 2016; published online 9 May 2016)
An orthogonalized flux-surface aligned curvilinear coordinate system has been developed from an
up-down asymmetric variation of the “Miller” flux-surface equilibrium model. It is found that
the new orthogonalized “asymmetric Miller” model representation of equilibrium flux surfaces
provides a more accurate match than various other representations of DIII-D [J. L. Luxon, Nucl.
Fusion 42, 614–633 (2002)] discharges to flux surfaces calculated using the DIII-D Equilibrium
Fitting tokamak equilibrium reconstruction code. The continuity and momentum balance equations
were used to develop a system of equations relating asymmetries in plasma velocities, densities,
and electrostatic potential in this curvilinear system, and detailed calculations of poloidal asymme-
tries were performed for a DIII-D discharge. Published by AIP Publishing.
[http://dx.doi.org/10.1063/1.4948552]
I. INTRODUCTION
The accuracy of calculations of poloidal asymmetries
from the fluid moment plasma equations in tokamak plasmas
can be improved by using flux-surface models that more
closely represent the true equilibrium surfaces. Early meth-
ods applied by Stacey to model elongated plasmas like DIII-
D (Reference 1) used a circular model which conserved outer
flux-surface area,2
and later models by Miller et al. intro-
duced a more complex formalism for explicitly modeling
up-down symmetric flux surfaces.3
Later, asymmetric varia-
tions of this Miller model further improved agreement with
equilibrium flux-surface shape predictions from the DIII-D
Equilibrium Fitting (EFIT) tokamak equilibrium reconstruc-
tion code.4
Incorporating this more accurate flux surface rep-
resentation into the plasma fluid equations allows the
influences of geometric asymmetries on poloidal asymme-
tries in plasma properties to be quantified.
In this analysis, the familiar “circular” analytic representa-
tion of flux-surface aligned curvilinear coordinate systems is
extended to incorporate an asymmetric variation of a “Miller”
plasma model and used to improve fluid model calculations of
plasma asymmetries in DIII-D. A general method for coordi-
nate system orthogonalization is presented, which can be easily
applied to develop magnetic field and scale factor representa-
tions using many other curvilinear models. A vertically asym-
metric form of a “Miller” representation of equilibrium flux
surfaces is shown to be the most accurate and efficient of the
four investigated methods of parameterizing flux surfaces in a
DIII-D shot. The magnetic field predictions based on scale fac-
tors formulated using these curvilinear models are compared
against calculations performed in a Cartesian system using an
experimentally based EFIT prediction for the Grad–Shafranov
equilibrium, confirming the improvement in accuracy obtained
using the asymmetric Miller model.
Numeric solution of a coupled set of moment equations
developed from the flux-surface averaged Fourier moments
of the continuity and momentum balance equations yields
calculations of plasma asymmetries in both the “circular”
model and “Miller” orthogonalized flux-surface aligned
coordinate systems. Comparison of these asymmetries illus-
trates the significant influence that improved plasma models
have on neoclassical asymmetry calculations.
II. ORTHOGONALIZED FLUX-SURFACE ALIGNED
CURVILINEAR COORDINATE SYSTEMS
Plasma calculations are performed using generalized cy-
lindrical coordinate systems with a basis vector directed in
the toroidal direction, allowing the assumption of tokamak
axisymmetry to reduce the calculations to 2D in a plane
describe by a plasma cross-section. Within this cross-
section, the remaining two basis vectors can be modeled as
fixed relative to the plasma center, directed perpendicular to
and parallel to the tokamak major axis. Alternatively, the
natural curvilinear coordinate system for calculations in
tokamak plasma is an orthogonal system oriented in the
poloidal and radial directions, changing orientation with
plasma position to remain directed parallel to and perpendic-
ular to plasma flux surfaces. This orthogonalized flux-
surface aligned (OFA) system can be developed from the
general flux-surface aligned (GFA) curvilinear covariant and
contravariant basis vectors5
[Figure 1].
The EFIT code6
solves the Grad–Shafranov equation for
a poloidal plasma cross-section in the radial and axial (R,Z)
dimensions of generalized cylindrical coordinates, yielding
distributions of F ¼ RB/ and of the scalar magnetic flux
function w. The toroidal component of the magnetic field
can be calculated by ~B/ ¼ F
R ^e/. The poloidal component of
the magnetic field can be related to spatial gradients of w by
~Bh ¼ 1
R rw  ^e/. Two mathematically equivalent forms of
this expression can be constructed by defining the gradient
a)
Now employed at Southern Nuclear Operating Company, Birmingham,
Alabama 35242. Electronic mail: tgcollar@southernco.com
1070-664X/2016/23(5)/052505/9/$30.00 Published by AIP Publishing.23, 052505-1
PHYSICS OF PLASMAS 23, 052505 (2016)
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3. operator in the ðR; ZÞ Cartesian plane of cylindrical coordi-
nates and in orthogonalized flux-surface aligned coordinates.
Poloidal Magnetic Field in Generalized Cylindrical
Coordinates:
jBhj ¼
1
R
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@w
@Z
2
þ
@w
@R
2
s
: (1)
Poloidal Magnetic Field in Orthogonalized Flux-Surface
Aligned Coordinates:
jBhj ¼
1
R
1
h?
q
@w
@q
: (2)
The magnetic flux function w is constant on flux surfaces, caus-
ing its poloidal gradient to vanish when h?
q is determined cor-
rectly. Consequently, the OFA expression for the magnitude of
the poloidal magnetic field simplifies to depend on only the ra-
dial gradient of w and the radial scale factor.
Distributions of the equilibrium flux function w through-
out a poloidal plasma cross-section were calculated by EFIT,
and analyzed and fitted to determine flux surfaces. Flux surfa-
ces of w ¼ constant and the central major radius ðR0Þ were
identified from the w distribution. Subsequently, the variation
of major radius ðRÞ and vertical elevation from the tokamak
midplane ðZÞ on each flux surface was fitted using 200-point
spline-fits; this had the added benefit of allowing gradients of
the poloidal component of the magnetic field Bh [Eq. (2)] to be
calculated analytically. Although this degree of accuracy in
flux-surface representation required mathematical complexity
which would not have been practical for representing position
or magnetic field in the plasma continuity and momentum bal-
ance equations, these spline fits were used as a basis for com-
paring the flux surface models discussed in Section III.
The covariant and contravariant basis vectors and the
scale factors for a general flux-surface aligned coordinate
system can be calculated;5
these basis vectors are not con-
strained to be orthogonal [Figure 2].
Covariant Basis Vectors:
~eq ¼
@R
@q
^eR þ
@Z
@q
^eZ; ~eh ¼
@R
@h
^eR þ
@Z
@h
^eZ;
~e/ ¼ R
@^eR
@/
¼ R^e/:
(3)
Covariant Scale Factors:
hq ¼ j~eqj ¼
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@R
@q
2
þ
@Z
@q
2
s
;
hh ¼ j~ehj ¼
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@R
@h
2
þ
@Z
@h
2
s
; h/ ¼ j~e/j ¼ R: (4)
Contravariant Scale Factors and Basis Vectors:
1
hq
¼ j~eq
j ¼
hh
H
;
1
hh
¼ j~eh
j ¼
hq
H
;
1
h/
¼ j~e/
j ¼
1
R
: (5)
Calculating the scalar triple product of the covariant
basis vectors yields the Jacobian for this system J ¼ Rð
@R
@q
@Z
@h À @Z
@q
@R
@h
0Þ. Dividing the Jacobian by the toroidal
covariant scale factor ðh/ ¼ RÞ produces an area scale
factor H ¼ J =R, which relates the poloidal cross-sectional
area of a differential element to differential changes in minor
radius (dq) and in poloidal angle (dh).
While the sets of covariant and contravariant unit
vectors of this general curvilinear system are not orthogonal,
covariant vectors are orthogonal with the opposing contra-
variant vectors. This property can be applied to construct an
orthogonalized flux-surface aligned coordinate system by
retaining the poloidal covariant basis vector, but selecting a
radial covariant basis vector aligned with the general radial
contravariant unit vector. Its magnitude is scaled so that
h?
q hh ¼ H ¼
^eqÂ^eh
dqdh
. The resulting scale factors for this
orthogonalized flux-surface aligned curvilinear coordinate
system can be expressed in terms of radial and poloidal
gradients of the cylindrical coordinate R and Z positions
[Eq. (6)]
FIG. 1. Cartesian, Cylindrical, and Flux-Surface Aligned Curvilinear coordi-
nate systems in a tokamak.
FIG. 2. Representative directions of covariant basis vectors ð~endn;
n ¼ ðq; hÞÞ, and contravariant unit vectors scaled by contravariant geometric
coefficients ð^en
hn
dn; n ¼ ðq; hÞÞ.
052505-2 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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4. h?
q ¼
@R
@q
@Z
@h
À
@Z
@q
@R
@h
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@R
@h
2
þ
@Z
@h
2
s0
@
1
A
À1
;
h?
h ¼ hh ¼
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@R
@h
2
þ
@Z
@h
2
s
; h?
/ ¼ h/ ¼ R: (6)
Using the radial scale factor in Eq. (6) to evaluate the expres-
sion for the poloidal field from Eq. (2) yields the expression
for the magnitude of the poloidal magnetic field in an orthog-
onal flux-surface aligned curvilinear coordinate system.
Bh ¼
1
R
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
@R
@h
2
þ
@Z
@h
2
s
@R
@q
@Z
@h
À
@Z
@q
@R
@h
À1
@w
@q
: (7)
III. ACCURACY OF ANALYTIC METHODS FOR
REPRESENTING CURVILINEAR COORDINATE
SYSTEMS
Various approximate analytic methods of expressing the
major radius R and vertical location Z of points in a tokamak
plasma in terms of flux-surface properties can be used to
simplify the calculations of Section II. A common model
represents the flux surfaces as circles about a fixed central
major radius ðR ¼ R0 þ r0 cos h; Z ¼ r0 sin hÞ, with flux-
surface dependent minor radii r0½qŠ ¼ aq. This equivalent
minor radius a is often approximated as constant throughout
the plasma,7
scaled so that the outer flux surface of the circu-
lar model approximates the surface area of an elliptical
plasma with elongation determined by EFIT. However, var-
iations of the circular model are incapable of modeling the
up-down asymmetries in the plasma minor radius, which
will influence the plasma flux-surface averaging operation.
A more advanced analytic plasma model capable of rep-
resenting the actual “D” shape of tokamak plasma was intro-
duced by Miller,3
and extended to up-down asymmetric
plasmas by Stacey7
R½q; hŠ ¼ R0 þ r0 cos n;
Z½q; hŠ ¼ j r0 sin hm; (8)
where n ¼ hm þ xd sin hm, hm is the Miller poloidal angle, r0
is the plasma-constant minor radius of the last closed flux
surface on the outboard midplane, j is the plasma elonga-
tion, and xd ¼ sinÀ1
d is the arcsine of the plasma triangular-
ity [Figure 3]. Radial profiles for j and d can be fitted from
the plasma EFIT data; the Stacey extension to the Miller
model (the Asymmetric Miller, AM) allows the elongation
and triangularity to be chosen separately for the upper and
lower plasma hemispheres. Because these quantities are radi-
ally dependent, their radial gradients must be taken into
account when calculating the gradients of the cylindrical
coordinate position @R
@q ; @Z
@q
.
Expressing the orthogonalized flux-surface aligned scale
factors and poloidal magnetic field in terms of the asymmet-
ric Miller model yields
h?
q ¼
a
1
a
@R0
@q
þ cos n
cos hm þ 1 þ
q
j
@j
@q
1 þ xd cos hmð Þ À q
@xd
@q
cos hm
sin n sin hm
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
cos2hm þ
1
j2
1 þ xd cos hmð Þ2
sin2
n
r
hh ¼ aq
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
j2 cos2hm þ 1 þ xd cos hmð Þ2
sin2
n
q
h/ ¼ R0 þ aq cos n (9)
and
Bh ¼
Bh
1 þ e cos n
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
cos2hm þ
1
j2
1 þ x cos hmð Þ2
sin2
n
r
1
a
@R0
@q
þ cos n
cos hm þ 1 þ
q
j
@j
@q
1 þ xd cos hmð Þ À q
@xd
@q
cos hm
sin n sin hm
; (10)
where the triangularity and elongation are discontinuous on
flux surfaces at the midplane, with constant values through-
out the upper and lower hemispheres [Figure 4]. It is worth
noting that the AM model can be extended beyond the pres-
ent upper-lower kappa/delta model to account for poloidally
dependent triangularity and elongation variations in the
FIG. 3. Miller model parameters relate major radius ðRÞ and vertical loca-
tion ðZÞ to the flux-surface dependent plasma elongation ðjÞ and triangular-
ity ðdÞ.
052505-3 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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2016 02:03:22
5. vicinity of the x-point. For analyses concerning the plasma
edge, this allows for an improved representation of the diver-
tor effects on the outer confined flux surfaces.
Besides the circular and Miller analytic plasma geome-
try models, two alternative methods of representing coordi-
nate systems using Fourier-expansion based fits of the EFIT
data were examined. The Single-Fourier (SF) model formal-
ism is identical to that of the circular model, but applies a
poloidally dependent minor radius represented using a
Fourier expansion
r½q; hŠ ¼ r0 1 þ
XN
n¼1
rc;n
cos n h þ
XN
n¼1
rs;n
sin n h
!
: (11)
The 0th order form of the single Fourier model reduces
to the circular model, with a radially dependent minor radius
which can be determined from the average minor radius of
the EFIT flux surfaces. Alternatively, a double Fourier model
(DF) applies two separate Fourier expansions to represent R
and Z
R½q; hŠ ¼ R0 þ
XN
n¼1
ðRs;n
sin n h þ Rc;n
cos n hÞ;
Z½q; hŠ ¼
XN
n¼1
ðZs;n
sin n h þ Zc;n
cos n hÞ: (12)
The accuracy of each model’s flux-surface representa-
tion as a function of flux surface location ðr½q; hŠÞ can be
approximated by comparison to the spline-fits discussed in
Section II ðrS½q; hŠÞ, using the radially dependent error metric
hjr q;h½ ŠÀrS q;h½ Šji
hrS q;h½ Ši for each flux surface. The average of this error
metric over the inner plasma ðq 0:7; q 2Þ is used in this
analysis as a metric of each model’s accuracy in describing
the inner region of the tokamak plasma [Table I].
The additional flexibility available with the Asymmetric
Miller model due to the extra fitting coefficients allows it to
be significantly more accurate than the circular model at rep-
resenting flux surfaces. Although the two Fourier-expansion
models have the potential for unlimited increase in accuracy
with higher order fits, the Asymmetric Miller model is more
accurate than both a 4th order single Fourier model and a
2nd order double Fourier model [Figure 5], while requiring
fewer coefficients to be fitted from EFIT flux-surface data
[Figure 6, left].
The formalism presented in Sec. III for expressing scale
factors and the poloidal component of magnetic field is gen-
eral enough to be used to represent the poloidal component
of the magnetic field in these different coordinate system
models. The accuracy of these magnetic field representations
can be compared to the poloidal magnetic field determined
by evaluating Equation (1) and interpolating the resulting
distribution to the flux surface locations determined by the
spline fit model ðBS
hÞ. The flux surface average of the differ-
ence between these field values
hjBhÀBS
h
ji
hBS
h
i
can also be calcu-
lated for each model, confirming that the asymmetric Miller
model is also significantly more accurate than the other mod-
els at representing the poloidal magnetic field [Figure 6,
right]. Its average over the central plasma ðq 0:7Þ can be
compared between models [Table I].
Comparing the field predictions from these systems
illustrates how the Asymmetric Miller OFA coordinate
system is the most accurate and efficient analytical represen-
tation of flux surface position [Figure 6, left]. It is also the
most accurate of the four analytic models considered at
representing the poloidal component of the magnetic field
[Figure 6, right].
FIG. 4. Elongations j (left) and triangularities d (right) for Symmetric Miller () and Asymmetric Miller upper and lower hemispheres (᭝, ٗ), determined by
least-squares fits to EFIT data for DIII-D discharge # 149468, 1905 ms.
TABLE I. Number of fitting coefficients required for each model, along
with averaged positional and field error
Model type
# Fitting
coefficients
per flux surface
% Average
positional error
ðq 0:7Þ
% Average
field error
ðq 0:7Þ
Curvilinear spline (CS) 400 … 0.22
Flux-equivalent circular (FC) 2 9.32 13.25
O(4) Single Fourier (SF) 10 0.38 1.07
O(2) Double Fourier (DF) 9 4.42 5.90
Asymmetric Miller (AM) 6 0.32 0.50
052505-4 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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6. IV. AN ASYMMETRIC PLASMA FLUID MODEL
The Asymmetric Miller model can be applied to the
plasma fluid momentum balance and continuity equations to
represent the effects of asymmetries in plasma geometry.
The particle distributions of electrons, deuterium ions, and
carbon ions can be modeled separately for the DIII-D
plasma, giving rise to a coupled set of equations describing a
three-species plasma.
The formalism from Section III can be applied to calcu-
late the scale factors and magnetic fields, allowing the inertial
terms and the magnetic forces to be directly determined from
the experimental configuration returned by the EFIT solution.
Adopting a simple Lorentz friction model ðFi;j ¼ Àni
mivi;jðVi À VjÞÞ allows the inter-ion frictional term to be
related to inter-species collision frequencies and mean parti-
cle velocities. The effects of friction between ions and elec-
trons are negligible in comparison to other forces, due to the
small electron mass. This small electron mass allows any
ion–electron, electron–ion, or electron–electron collision fre-
quency to either be approximated as independent of particle
mass, or to scale as melec=mion [Eq. (13)]
i;j ¼
1
6
ffiffiffi
2
p
p3=22
0
nje2
i e2
j
ffiffiffiffiffiffi
li;j
p
ln Ki;j
 Ã
miT3=2
: (13)
A Braginskii viscosity model8
[Eq. (14)] with parallel
viscosity coefficients g0;i ¼ 2 niTi
i;i
fi
developed for the colli-
sionless plasma regime via a viscosity interpolation fið
¼
^i;i
2
e3=2þ^i;ið Þ 1þ^i;ið Þ
; ^i;i ¼ i;i
qR0
Vth;i
Þ9,10
can be used to express
the ion viscosity in terms of gradients of mean particle veloc-
ities, densities, and magnetic fields
Pa;b ¼ P0
a;b þ P12
a;b þ P34
a;b
¼ Àg0W0
a;b À ðg1W1
a;b þ g2W2
a;bÞ þ ðg3W3
a;b þ g4W4
a;bÞ;
Wc
a;b ¼ f½~B; ~VŠ: (14)
FIG. 5. Representative flux surfaces
for fitted Asymmetric Miller and Flux-
surface equivalent Circular models
(left), and the Single Fourier and
Double Fourier models (right), as com-
pared to the reference EFIT surfaces.
FIG. 6. Flux Surface Averaged positional error (left) and field error (right) for four analytic plasma geometry models.
052505-5 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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7. The elements of this viscosity tensor in an asymmetric toka-
mak with
jB/j
jBj ffi 1 and jBhj
jBj ( 1 have been developed for
orthogonalized flux-surface aligned coordinate systems,9,11
and are applied in this analysis. Braginskii’s form for the
gyroviscosity can be used, as it is independent of plasma col-
lisionality g3;i ¼ 1
2 g4;i; g4;i ¼ niTi
Xi
.8
In comparison to the
parallel and gyroviscous terms, the perpendicular viscosity is
negligibly small ðg0 ) g3;4 ’ g0=Xs ) g1;2 ’ g0=ðXsÞ2
Þ.
The remaining equations comprise a coupled set of
three-species equations, relating the electric potential to the
densities, velocities, and temperatures of electrons, deute-
rium, and carbon. This analysis is simplified by assuming
thermal equilibrium between deuterium and carbon and con-
stant temperatures on flux surfaces, allowing the ion and
electron temperature distributions to be set directly from
radially dependent experimental measurements.12
Both the
electron density and the deuterium radial velocity are also
assumed to be constant on flux surfaces; the electron density
is set from experimental Thompson-scattering measure-
ments, and the deuterium continuity equation can be used to
express the deuterium radial velocity in terms of the neutral-
beam particle source calculated by ONETWO.13
Because
there is no internal source of carbon to the plasma, the car-
bon radial velocity can be neglected. The external source of
toroidal momentum due to neutral beam injection of deute-
rium is also calculated by ONETWO; the carbon momentum
sources and deuterium momentum sources in poloidal and
radial directions are negligibly small.
The remaining seven distributions of electric potential
and ion densities, poloidal velocities, and toroidal velocities
are modeled in this analysis using separation of variables,
and low-order Fourier expansions to represent the poloidal
dependence
x½q; hŠ ¼ x½qŠ~x½hŠ;
~x½hŠ ¼ 1 þ
XN
n¼1
ðxs;n
sin n h þ xc;n
cos n hÞ:
(15)
This method allows for the poloidal variations of these
quantities on flux surfaces to be approximated to first order
in terms of their sine/cosine “asymmetries,” which express
the magnitude of poloidal variations in relation to the
mean values of plasma quantities on flux surfaces.
Although this formalism breaks down in regions where the
mean values are very small, it has been frequently applied
as a fairly robust way of ordering the plasma equations
towards the central, collisionless region of tokamak
plasmas.11,14
V. SYSTEM OF NONLINEAR PLASMA FLUID
EQUATIONS RELATING POLOIDAL ASYMMETRIES
As this analysis focuses on how the asymmetric Miller
model influences plasma asymmetries, the mean values of
the seven asymmetric distributions are set from experimental
measurements and approximations based on experimental
measurements. Charge neutrality is used to relate the density
distribution of deuterium to those of carbon and electrons,
which can both be directly measured. Experimental measure-
ments of carbon toroidal and poloidal velocities are com-
monplace in DIII-D; however, shot 149468 was designed
also to allow for measurements of the toroidal component of
deuterium velocity. This allowed the poloidal component of
deuterium velocity to be calculated using the deuterium ra-
dial momentum balance.12
Finally, the carbon radial momentum balance can be
used to express the electric potential in terms of the car-
bon velocities, the pressure gradient, and the magnetic
field
1
h?
q
@vpcb
@q
g h½ Š
* +
¼ ecnc À
1
h?
q
@U
@q
þB/Vh;c ÀBhV/;c
!
g h½ Š
* +
:
(16)
A coupled set of equations relating the fourteen sine
and cosine asymmetries in electric potential, ion densities,
and both poloidal and toroidal components of ion velocities
can be constructed from the flux-surface averages hCið
¼ 2p
Vq
Þ
h C h?
q hhh/dhÞ of the sine and cosine moments
ðg½hŠ ¼ sin h; cos hÞ of the poloidal component of the elec-
tron momentum balance (the Maxwell–Boltzmann equation)
[Eq. (17)], the ion continuity equations [Eq. (18)], the ion
poloidal momentum balance equations [Eq. (19)], and the
ion toroidal angular momentum balance equations [Eq.
(20)]. Although the orthogonality of Fourier basis functions
allows for some analytical simplification of these fourteen
moment equations, the added complexity necessary in order
to retain the non-linear asymmetric Miller formalism
resulted in analytical calculations of the flux-surface aver-
ages of the Fourier moment equations being impractical.
Instead, the elements of these flux-surface averaged equa-
tions were calculated numerically using the Magneto-
Hydrodynamic Tokamak Rotation (MHTR) code,9
which
then solves the coupled set of fluid moment equations using
a hybrid Mathematica-Fortran solution method. This numer-
ical model applies an iterative Fortran matrix-inversion rou-
tine to solve a linearized system of the fourteen flux-surface
averaged plasma equations described above at 50 radial
mesh locations. The matrix form of this system of fourteen
equations is generated using Mathematica. Any of the four
coordinate system models discussed above can be used to
set scale factors and magnetic fields, which allows for com-
parison of the asymmetries calculated in each coordinate
system.
Electron Momentum Balance:
1
hh
@vpeb
@h
g h½ Š
( )
¼ eene À
1
hh
@U
@h
g h½ Š
( )
: (17)
Ion Continuity:
1
hhh?
q h/
@vVr;inihhh/b
@q
þ
@vVh;inih?
q h/b
@h
!
g h½ Š
* +
¼ hS0
i g h½ Ši:
(18)
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8. Ion Poloidal Momentum Balance:
mi
g h½ Š
h2
hh?
q h/
@vVh;iVr;inih/h2
hb
@q
þ
g h½ Š
hhh?
q h/
@vV2
h;inih/h?
q b
@h
*
Àni
V2
r;i
hhh?
q
@h?
q
@h
þ
V2
/;i
hhh/
@h/
@h
!
g h½ Š
+
þ
g h½ Š
hhh?
q h/
@vPh;hh?
q h/b
@h
*
À
g h½ Š
hhh?
q
@h?
q
@h
Pr;r À
g h½ Š
hhh/
@h/
@h
P/;/
+
þ
1
hh
@vpib
@h
g h½ Š
( )
¼ eini À
1
hh
@U
@h
ÀB/Vr;i
g h½ Š
( )
þhmini Vh;i ÀVh;jð Þi;jg h½ Ši:
(19)
Ion Toroidal Angular Momentum Balance:
mi
hhh?
q h/
@vV/;iVr;inih2
/hhb
@q
þ
@vV/;iVh;inih2
/h?
q b
@h
!
g h½ Š
* +
þ
1
hhh?
q h/
@vPr;/h2
/hhb
@q
þ
@vPh;/h2
/h?
q b
@h
!
g h½ Š
* +
¼ h/eini À
@vA/b
@t
þ BhVr;i
g h½ Š
( )
þ hh/mini V/;i À V/;jð Þi;jg h½ Ši þ hh/S1
/;ig h½ Ši: (20)
MHTR solves the final coupled set of fourteen fluid
moment Magneto-Hydrodynamic Tokamak Rotation equa-
tions by iteratively converging the solution of linearized
forms of the Fourier moment equations until the normalized
residuals are reduced below a target value of 0.001% for flux
surfaces with q 0:7. In addition to this coupled set of equa-
tions, MHTR also solves for averaged electric potential and
deuterium radial velocity consistent with the asymmetry
equations using the nonlinear forms of the radial momentum
balance and the deuterium continuity equation. The asymme-
tries in plasma properties have only quadratic effects on
these radial profiles of electric potential and radial deuterium
velocity.
Because the method of representing plasma asymme-
tries applied here requires that asymmetries be normalized
by mean velocities, the formalism presented in this analy-
sis is only valid for plasma regions where the plasma mean
velocity is non-zero. For the particular shot considered, the
formalism does not converge when the mean deuterium
poloidal velocity reverses direction around the q ¼ 0:75
flux surface. Thus, the results of this analysis are only pre-
sented for mesh locations where q 0:7. This is consistent
with the metrics used to show the influences of flux surface
models on position and poloidal field calculations in
Section II, which were averaged over the inner flux surfa-
ces. Improving the methodology used to represent the
plasma distribution functions [Eq. (15)] to use un-
FIG. 7. Asymmetric Miller model calculations of sine and cosine plasma asymmetries.
052505-7 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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2016 02:03:22
9. normalized asymmetries shows potential for extending this
formalism over all plasma regions.
VI. CALCULATED POLOIDAL ASYMMETRIES IN A
DIII-D DISCHARGE
The hybrid MHTR code is applied to calculate asymme-
tries using the circular and asymmetric Miller models. To
illustrate the effect of the orthogonalization technique on the
asymmetries, asymmetries are also calculated using only co-
variant and only contravariant scale factors—effectively
overestimating and underestimating the flux-surface vol-
umes. The asymmetries calculated using the asymmetric
Miller model are shown in Figure 7.
The radial average of the normalized percent difference
from the Asymmetric Miller (AM) model calculations
j~xÀ~xAMj
j~xAMj
is computed for each asymmetry in the circular,
covariant, and contravariant models. The average of this
quantity for q 0:7 is representative of the accuracy of the
asymmetry calculations in each of these three models, as
compared to the calculations performed using the
Asymmetric Miller model.
The largest percent differences from the AM asymme-
tries, as determined by this metric, occur for the four asym-
metries in poloidal velocity, averaging around 107%, 55%,
and 4% for difference between asymmetries calculated using
the AM geometry and asymmetries calculated using a circu-
lar model, an AM model with only covariant scale factors,
and an AM model with only contravariant scale factors,
respectively. The differences are especially extreme in the
deuterium asymmetries; this is primarily due to the very
small average size of the comparison AM model asymme-
tries [Figure 8].
The averaged difference from the Asymmetric Miller
asymmetries for the remaining ten asymmetries in toroidal
velocity (four), density (four), and electric potential (two) is
23% for the circular model, 4% for the covariant AM, and
3% for the contravariant Miller. The overall averaged differ-
ences from the AM model in the final asymmetries calcu-
lated using each of the three models are 47%, 19%, and 3%.
VII. CONCLUSION
A technique for orthogonalizing general flux-surface
models has been developed, which provides a straightfor-
ward way to incorporate an improved-accuracy asymmetric
form of the “Miller” equilibrium flux-surface model into the
plasma fluid moment equations through scale factors and the
model for the poloidal magnetic field. Flux surfaces fitted
using the asymmetric “Miller” flux surface aligned
FIG. 8. Sine (left) and Cosine (right) asymmetries in Poloidal Velocity for Deuterium (top) and Carbon (bottom), calculated using the Asymmetric Miller
model (᭛), Flux-surface conserving circular model (᭺), purely Covariant Asymmetric Miller (x), and purely Contravariant Asymmetric Miller (þ).
052505-8 T. G. Collart and W. M. Stacey Phys. Plasmas 23, 052505 (2016)
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2016 02:03:22
10. curvilinear coordinate system match comparable equilibrium
plasma surfaces computed using EFIT with an average of
0.32% error, as compared to the 9.3% average error associ-
ated with the circular model. Using the divergence of the
magnetic flux function w to predict the poloidal magnetic
field yields agreement with EFIT calculations to within 0.5%
for the orthogonalized form of the asymmetric Miller plasma
model inside the q ¼ 2 flux surface, also a significant
improvement over the 13.3% error when using the circular
model.
Calculations of plasma asymmetries using Fourier
moments of the deuterium and carbon continuity equations
and components of the momentum balance equations change
by an average of 47% when switching between scale factors
modeled in the circular versus the orthogonalized asymmet-
ric Miller model. This confirms that improvements in the
plasma geometry model do influence fluid equation calcula-
tions. The differences due to neglecting the orthogonaliza-
tion technique and applying only the Asymmetric Miller
covariant or only contravariant scale factors are generally
less pronounced, but still significant enough to illustrate the
necessity of using scale factors derived from an orthogonal
coordinate system.
All radial calculations of asymmetries show a trend of
increasing in magnitude with increasing minor radius.
Carbon sine and cosine asymmetries in density, poloidal
velocity, and toroidal velocity are much larger than deute-
rium asymmetries, with magnitudes greater than 10%.
Cosine asymmetries in deuterium toroidal and poloidal
velocity are still significant, though with normalized asym-
metries approaching 10% towards the edge. However, the
accuracy of these calculations of asymmetries outside of the
plasma center is limited by the assumption of separation of
variables and by the use of only first order Fourier series to
approximate the distributions of plasma properties. Because
even a fourth-order Fourier series was still unable to attain
the accuracy of the Asymmetric Miller model at matching
the plasma geometry, it may be necessary in future analyses
to represent the plasma properties with at least this order of
Fourier series, despite the additional complexity and calcula-
tion time that this would add to MHTR.
These predictions of poloidal asymmetries have
applications in the fluid moment modeling of toroidal gyro-
viscosity,14,15
and on modeling of tokamak impurity trans-
port.16
Although further improvements should be made to
increase the accuracy of the formalism applied by MHTR,
the difference between asymmetry calculations due to coor-
dinate system improvements indicates that the circular model
alone is not sufficient for performing this type of analysis,
due to its inability to model the plasma up-down asymme-
tries, and that more advanced plasma geometry models such
as the Asymmetric Miller should be applied.
ACKNOWLEDGMENTS
The authors are grateful to B. A. Grierson for providing
the DIII-D data. This work was supported in part by the U.S.
Department of Energy under Grant No. FE-F601-ER54538
with the Georgia Tech Research Corporation, and in part by
Southern Nuclear Operating Company.
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2016 02:03:22