Perl 6 is here today ... for some uses, like writing parsing scripts, that would be too complicated for a single Perl 5 regex. This is an overview what has changed.
This figure, created in June 2013, is taken from the Final Petroleum Hydrocarbon Project Work Plan, Parcel C, Hunters Point Naval Shipyard, San Francisco, California. It displays isoconcentration contours for a total petroleum hydrocarbon plume in groundwater that are based on the contaminant concentrations reported on the figure.
Part of the Fluid Mechanics curriculum at Cal Poly Pomona was to analyze the performance of a centrifugal pump and generate a report of the relevant results.
Perl 6 is here today ... for some uses, like writing parsing scripts, that would be too complicated for a single Perl 5 regex. This is an overview what has changed.
This figure, created in June 2013, is taken from the Final Petroleum Hydrocarbon Project Work Plan, Parcel C, Hunters Point Naval Shipyard, San Francisco, California. It displays isoconcentration contours for a total petroleum hydrocarbon plume in groundwater that are based on the contaminant concentrations reported on the figure.
Part of the Fluid Mechanics curriculum at Cal Poly Pomona was to analyze the performance of a centrifugal pump and generate a report of the relevant results.
This presentation was made for CSE student to understand easily quick sort algorithm to implement quick algorithm. So if u want to learn quick sort than watch it.
Chato low gravity cryogenic liquid acquisition for space exploration 2014David Chato
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NASA is currently developing propulsion system concepts for human exploration. These propulsion concepts will require the vapor free acquisition and delivery of the cryogenic propellants stored in the propulsion tanks during periods of microgravity to the exploration vehicles engines. Propellant management devices (PMDβs), such as screen channel capillary liquid acquisition devices (LADβs), vanes and sponges currently are used for earth storable propellants in the Space Shuttle Orbiter and other spacecraft propulsion systems, but only very limited propellant management capability currently exists for cryogenic propellants. NASA is developing PMD technology as a part of their cryogenic propellant storage and transfer (CPST) project. System concept studies are looking at the key factors that dictate the size and shape of PMD devices and established screen channel LADs as an important component of PMD design. Normal gravity experiments and modeling are studying the behavior of the flow in LAD channel assemblies (as opposed to only prior testing of screen samples ) at the flow rates representative of actual engine service. Recently testing of LAD channels in liquid Hydrogen was completed. Three different types of test were conducted: Measurement of the pressure drop for flow through a one inch diameter screen sample; Measurement of the pressure drop in a horizontally-mounted rectangular LAD channel assembly at flow rates representative of a main engine firing; and determination of bubble breakthrough for flow into a partially-immersed vertically-mounted LAD channel. This presentation will present an overview of low gravity cryogenic liquid acquisition strategies, review the findings of this recent test series, and discuss the implications of the testing and studies to exploration mission concepts.
Calibration of A Five-Hole Probe in Null and Non-Null Technique IJERA Editor
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The analysis of fluid flow is encountered in almost all engineering applications. Flow measurements,
particularly velocity and its direction, turbulence quantities are needed in order to improve the understanding of
various complex flow phenomena and to validate and further refine the computer flow models. Pressure probes
find wide application in the measurement of fluid flows both in the laboratory and in the industry. A five-hole
pressure probe is calibrated in both null and non-null technique. An algorithm for five-hole probe in non-null
method is developed which utilizes a database of calibration data and a local least-squares interpolation
technique is used for interpolation of flow properties. It is also found out that the non-null method was superior
in ease of use and prediction of flow measurement variables than the null method.
MATHEMATICAL MODELLING FOR ANALYSIS OF CHANGE IN SHAPE OF SUCTION MANIFOLD TO...ijiert bestjournal
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Centrifugal pumps are used extensively for pumping water over short to medium distance through pipeline where the requirements of head and discharge are moderate. The design and optimization of turbo machine impellers such as tho se in pumps and turbines is a highly complicated task due to the complex three-dimension al shape of the impeller blades and surrounding devices. Small differences in geometry can lead to significant changes in the performance of these machines. The efficiency of th e centrifugal pump can be increased by number of ways such as modifying the geometry of th e sump,increasing the diameter of the suction pump,having multiple pumps working in seri es,etc. This paper is part of research work carried out to improve efficiency of a centrifugal pump through changing shapes of the manifolds.
Similar to Pressure drop model presentation april 19th (20)
MATHEMATICAL MODELLING FOR ANALYSIS OF CHANGE IN SHAPE OF SUCTION MANIFOLD TO...
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Pressure drop model presentation april 19th
1. CHE 4002-401 Chemical Engineering Laboratory I: Project III
Oklahoma State University
Coach Clint Aichele
Coach Mike Resetarits
Coach Russ Rhinehart
13. π2 = πΎ π§3 β π§2 + π
πΏ
π·
+ πΎπΏ
8π2
ππ2 π·4
Sketch to illustrate the points (2) and (3)
14. N plates
6 psig
Record Flow Rate in 1 min
Calculate P2
Repeat with new filter papers
*N = 8, 12, and 16
Number of Plates:
Inlet Pressure (P1): 9 psig 12 psig
15. 14 plates
Proper Orientation
Record Flow Rate in 1 min
Calculate P2
Number of Plates:
Inlet Pressure Range (P1): 3 β 12 psig
Random Orientation
16.
17.
18.
19. βπππππππππ= π +
π
π
β π + π +
π
π π
β π π
4.50
5.00
5.50
6.00
6.50
7.00
7.50
8.00
8.50
9.00
9.50
10.00
10.50
11.00
11.50
12.00
12.50
13.00
3.8 4 4.2 4.4 4.6 4.8 5 5.2 5.4 5.6 5.8 6 6.2 6.4 6.6
P1-P2
(psig)
Flow Rate Q (gal/min)
Pressure drop vs. Flow rate when N=8
Data Model
Laminar Model
Turbulent Model
Combined Model
20. 3.00
3.50
4.00
4.50
5.00
5.50
6.00
6.50
7.00
7.50
8.00
8.50
9.00
9.50
10.00
10.50
11.00
4.5 5 5.5 6 6.5 7 7.5 8 8.5 9
P1-P2(psig)
Flow rate Q (gal/min)
Pressure drop vs. Flow rate when N=14
Process Model
Data Model
3.00
3.50
4.00
4.50
5.00
5.50
6.00
6.50
7.00
7.50
8.00
8.50
9.00
9.50
10.00
10.50
11.00
4.2 4.7 5.2 5.7 6.2 6.7 7.2 7.7 8.2 8.7
P1-P2(psig)
Flow rate Q (gal/min)
Pressure drop vs. Flow rate when N=14
Data Model
Process Model