The document discusses project management methodologies, specifically comparing traditional waterfall and agile approaches. It provides details on waterfall, including its sequential phases of requirements, design, implementation, and test. Agile methodologies are described as iterative with short development cycles. The Scrum framework is then explained in depth, covering its roles of Product Owner, Scrum Master, and team, along with artifacts like the Product Backlog, Sprint Backlog, and burndown chart. Key Scrum meetings like the Sprint Planning, daily standup, and Sprint Review meetings are also outlined.
The document discusses project risk management over 7 days. Day 5 focuses on project risk management and includes discussions of identifying risks, qualitative and quantitative risk analysis, and planning risk responses. Key topics covered are the importance of risk management, types of risks, tools for risk identification like brainstorming, risk breakdown structures, and risk registers to document risks.
The document provides an outline for a project management course. It includes details on the topics that will be covered each day, including project integration management, scope management, schedule management, cost management, risk management, and Scrum. The focus of the specific section summarized is on project cost management. It defines key processes involved in project cost management like planning, estimating, budgeting, controlling, and managing costs. Formulas for earned value management are also provided to measure project performance and forecast estimates.
The document discusses project schedule management processes including plan schedule management, define activities, sequence activities, estimate activity resources, and estimate activity durations. It provides details on each process, including inputs, tools and techniques, and outputs. The key steps are decomposing work into activities, defining relationships between activities, estimating resource needs and duration of each activity, and developing a project schedule network diagram.
The document outlines a 7-day project management training course. Day 1 covers an introduction to project integration management. Later days cover additional topics like scope, schedule, cost, risk management and Scrum. The course aims to help participants understand key project management principles, processes, knowledge areas and the role of the project manager. It emphasizes the importance of integrating all project efforts, balancing scope, time and cost constraints, and addressing stakeholder needs.
The document outlines the course schedule for a 7-day project management training. Day 2 focuses on project scope management. It defines key scope management terms and processes. The presentation covers planning scope management, collecting requirements, defining the scope statement, creating the work breakdown structure (WBS), and validating scope. Tools for collecting requirements and creating the WBS are also discussed.
This document provides guidance on writing a business plan. It explains that a business plan clarifies the feasibility of a business idea by evaluating the potential market, management team, and profitability. It also communicates the idea to investors and provides the basis for securing financing. The document outlines the typical sections of a business plan, including executive summary, business description, products/services, sales and marketing plan, operations plan, and financial projections. It emphasizes that a well-written business plan is important for gaining investor confidence and improving the chances of business success.
This document appears to be a presentation about cyber-physical systems and Industry 4.0. It includes definitions of cyber-physical systems and Industry 4.0, examples of companies implementing Industry 4.0 solutions, discussions of the Internet of Things, impacts of new technologies on the economy, business, society and individuals, and slides on various related topics without titles like applications, history, and use cases. The presentation touches on many aspects of emerging digital technologies and their integration with physical systems and processes.
The document discusses project management methodologies, specifically comparing traditional waterfall and agile approaches. It provides details on waterfall, including its sequential phases of requirements, design, implementation, and test. Agile methodologies are described as iterative with short development cycles. The Scrum framework is then explained in depth, covering its roles of Product Owner, Scrum Master, and team, along with artifacts like the Product Backlog, Sprint Backlog, and burndown chart. Key Scrum meetings like the Sprint Planning, daily standup, and Sprint Review meetings are also outlined.
The document discusses project risk management over 7 days. Day 5 focuses on project risk management and includes discussions of identifying risks, qualitative and quantitative risk analysis, and planning risk responses. Key topics covered are the importance of risk management, types of risks, tools for risk identification like brainstorming, risk breakdown structures, and risk registers to document risks.
The document provides an outline for a project management course. It includes details on the topics that will be covered each day, including project integration management, scope management, schedule management, cost management, risk management, and Scrum. The focus of the specific section summarized is on project cost management. It defines key processes involved in project cost management like planning, estimating, budgeting, controlling, and managing costs. Formulas for earned value management are also provided to measure project performance and forecast estimates.
The document discusses project schedule management processes including plan schedule management, define activities, sequence activities, estimate activity resources, and estimate activity durations. It provides details on each process, including inputs, tools and techniques, and outputs. The key steps are decomposing work into activities, defining relationships between activities, estimating resource needs and duration of each activity, and developing a project schedule network diagram.
The document outlines a 7-day project management training course. Day 1 covers an introduction to project integration management. Later days cover additional topics like scope, schedule, cost, risk management and Scrum. The course aims to help participants understand key project management principles, processes, knowledge areas and the role of the project manager. It emphasizes the importance of integrating all project efforts, balancing scope, time and cost constraints, and addressing stakeholder needs.
The document outlines the course schedule for a 7-day project management training. Day 2 focuses on project scope management. It defines key scope management terms and processes. The presentation covers planning scope management, collecting requirements, defining the scope statement, creating the work breakdown structure (WBS), and validating scope. Tools for collecting requirements and creating the WBS are also discussed.
This document provides guidance on writing a business plan. It explains that a business plan clarifies the feasibility of a business idea by evaluating the potential market, management team, and profitability. It also communicates the idea to investors and provides the basis for securing financing. The document outlines the typical sections of a business plan, including executive summary, business description, products/services, sales and marketing plan, operations plan, and financial projections. It emphasizes that a well-written business plan is important for gaining investor confidence and improving the chances of business success.
This document appears to be a presentation about cyber-physical systems and Industry 4.0. It includes definitions of cyber-physical systems and Industry 4.0, examples of companies implementing Industry 4.0 solutions, discussions of the Internet of Things, impacts of new technologies on the economy, business, society and individuals, and slides on various related topics without titles like applications, history, and use cases. The presentation touches on many aspects of emerging digital technologies and their integration with physical systems and processes.
This document discusses shear flow in aircraft structural design. It covers governing equations for shear flow calculations, case studies of shear flow in aircraft fuselages, and methods for calculating moments of inertia and shear flow. The document is a lecture on shear flow given by Dr. Mohamed Elfarran of Cairo University's Aerospace Engineering Department.
The document discusses analyzing the ultimate bending strength of an aircraft fuselage structure. It provides an example problem to calculate the ultimate bending moment of a fuselage cross section considering shear lag and inter-rivet buckling effects. The solution involves determining the effective area of structural elements through an iterative process accounting for stresses, strains, and shear lag factors. The example provides details of the fuselage geometry, materials, and step-by-step working to arrive at the ultimate bending moment and stringer forces.
This document discusses calculating the ultimate bending strength of a fuselage structure. It provides an example problem of determining stresses in the stringers and skin of a fuselage cross-section due to an applied bending moment. The solution involves iteratively calculating the neutral axis position and effective area through trial and error, starting with an initial assumption that all materials are effective in tension. The results of the first trial are then used to refine the model for a second trial. Comparing the results shows an error of 14% in the neutral axis position between the first and second trials.
The document discusses three cases of aircraft structural loading and the resulting stresses: 1) Pressurization of the fuselage shell, which induces longitudinal and circumferential stresses that depend on the material properties and geometry, 2) Torsional loading of the fuselage shell, which causes shear stresses proportional to the applied torque and cross-sectional properties, and 3) Bending loads on wing spars, which are resisted by shear stresses in the spar webs and normal stresses in the spar caps that depend on the bending moment and section properties.
This document discusses analyzing stresses on an unsymmetrical tapered fuselage structure due to applied loads. It provides an example problem to determine stringer stresses and forces at two stations, section 0 and section 30, given loads applied at station 150. The solution strategy is outlined, which involves using the general bending stresses equation and calculating the centroid position with respect to the Z and Y axes. Steps are shown for calculating stresses at each section.
This document discusses material properties and bending stresses. It defines key terms like modulus of elasticity, Poisson's ratio, yield stress, and ultimate tensile stress. It explains that plane sections remain plane after bending but rotate, and that the neutral axis experiences no deformation or stress. The location of the neutral axis depends on the material properties and loading conditions. Equations are provided to calculate bending stresses based on the neutral axis location and applied moment. An example problem calculates bending stresses at different points on an airplanes wing. The document also notes that for very high loads above the elastic range, stresses become nonlinear and the neutral axis must be determined through trial and error.
The document outlines a lecture on fuselage structural design. It discusses iterative methods for calculating effective width and radius of gyration of thin-walled structures. It also covers loads acting on the fuselage, fuselage structure components like stringers and frames, and examples of analyzing stresses in circular fuselage sections. The document concludes by mentioning that stress analysis of wings will be covered next.
This document discusses effective sheet width and inter-rivet buckling in aerospace structures. It explains that stringers stiffen wing and fuselage skins, and skins provide stiffness to stringers even when buckling. An effective width calculation accounts for this effect. The document also describes how inter-rivet buckling can occur if rivet spacing is too long, and provides equations to calculate the effective rivet spacing to prevent this issue.
The document discusses the design of aircraft fuselages. It notes that fuselages must house passengers and luggage with proper strength and light weight. Fuselages experience both distributed and concentrated loads from various sources. A circular cross-section is commonly used as it efficiently handles these loads. Fuselage structures typically consist of a thin-walled tube with transverse frames, stringers, and cutouts. The document provides an example problem calculating the ultimate bending strength of a circular fuselage cross-section made of aluminum with stringers of different sizes. It considers linear and nonlinear stress distributions to determine the maximum moment the fuselage can withstand before failure.
- The fuselage skin consists of curved sheet panels that can buckle if no stiffeners are present. Stiffener elements are needed to calculate and compare the buckling loads to the aircraft's ultimate loads.
- Buckling of aircraft structures like fuselage skins must be analyzed and prevented. Curved sheets and cylinders can buckle under compression, bending, shear, torsion and combined loads. Internal pressure increases the buckling strength.
- Design examples are provided to calculate buckling loads of circular cylinders and curved-stiffened sheets under various loading conditions and determine if panels would buckle. Buckling analysis ensures the structure can withstand required loads.
1. The document discusses stresses in thin-walled and thick-walled cylinders. For thin-walled cylinders, the stress is assumed to be uniform throughout the wall. For thick-walled cylinders, the stresses depend on the radius and include circumferential (hoop), radial, and longitudinal stresses.
2. Internally pressurized thick-walled cylinders experience maximum hoop stress and compressive radial stress at the inner surface. The hoop stress decreases and radial stress increases towards zero at the outer surface. Longitudinal stress is uniform across the wall.
3. Externally pressurized thick-walled cylinders experience minimum hoop stress and compressive radial stress at the outer surface
This document provides an overview of various gear types and gear terminology. It discusses spur gears, helical gears, bevel gears, worm gears, and compares their basic configurations. Key gear concepts covered include involute tooth profiles, conjugate action, pressure angle, pitch circle, circular pitch, diametral pitch, addendum, dedendum, interference, contact ratio, and gear forming/cutting methods. Standard tooth systems and proportions are also presented in tables.
This document provides an overview of helical spring design and analysis. It discusses stresses in helical springs, deflection calculations, compression spring types, stability, materials selection, static design considerations, critical frequencies, and examples. The chapters cover key topics like curvature effects, stresses from torsion and shear, deflection-force relationships, buckling analysis, material properties, recommended design ranges, and the wave equation for vibrational frequency.
This document discusses threaded fasteners and screw threads. It defines common screw thread parameters like pitch, major diameter, and thread angle. It describes metric and unified screw thread standards. It also discusses power screws, different types of threaded fasteners, and how to select the proper fastener for an application based on required load and functional parameters.
The document discusses analyzing the stresses and deflections in aerospace shell beam structures like aircraft wings and space habitats. It presents an approach to idealize the cross-section into parts that carry extensional stress from bending and axial loads versus parts that carry shear stress from shear loads and torques. Joint equilibrium equations are developed and the problem is broken into "pure shear" and "pure torsion" cases that are then summed using superposition. Deflections are also analyzed by summing contributions from bending, shearing, and torsion.
The document discusses shear flow analysis of cantilevered wings. It presents equilibrium equations for 1-cell and 2-cell cantilevered wing models. Tables show shear flow analysis results for a 2-cell cantilevered wing with properties such as shear, bending moment, and torque calculated at each cell. Shear correction factors are also discussed.
This document outlines material properties testing methods and concepts. It discusses tensile testing to determine material strengths, stress-strain diagrams, elastic modulus, resilience, toughness, statistical variation in properties, effects of temperature and cold working. It also summarizes material classes including metals, plastics, composites and provides examples of common materials like steels, aluminum, titanium, polymers. Key material properties like strengths, moduli and factors affecting properties are defined.
This document discusses shaft design and layout. It covers selecting materials for shafts, including steel alloys. Geometric layout is discussed, including supporting axial loads and transmitting torque. Common shaft components like keys, pins, and set screws are described. Stress analysis equations for bending and torsion are provided. Estimating stress concentrations at features like shoulders is covered. The document contains many diagrams illustrating shaft configurations and components.
This document provides an overview of spring design and analysis. It discusses various types of springs including compression springs, extension springs, and torsion springs. It covers topics such as stresses in springs, deflection calculations, stability, materials selection, design considerations, fatigue loading, and critical frequencies. The document is presented in a series of slides intended for a lecture on spring design.
This document discusses shear flow in aircraft structural design. It covers governing equations for shear flow calculations, case studies of shear flow in aircraft fuselages, and methods for calculating moments of inertia and shear flow. The document is a lecture on shear flow given by Dr. Mohamed Elfarran of Cairo University's Aerospace Engineering Department.
The document discusses analyzing the ultimate bending strength of an aircraft fuselage structure. It provides an example problem to calculate the ultimate bending moment of a fuselage cross section considering shear lag and inter-rivet buckling effects. The solution involves determining the effective area of structural elements through an iterative process accounting for stresses, strains, and shear lag factors. The example provides details of the fuselage geometry, materials, and step-by-step working to arrive at the ultimate bending moment and stringer forces.
This document discusses calculating the ultimate bending strength of a fuselage structure. It provides an example problem of determining stresses in the stringers and skin of a fuselage cross-section due to an applied bending moment. The solution involves iteratively calculating the neutral axis position and effective area through trial and error, starting with an initial assumption that all materials are effective in tension. The results of the first trial are then used to refine the model for a second trial. Comparing the results shows an error of 14% in the neutral axis position between the first and second trials.
The document discusses three cases of aircraft structural loading and the resulting stresses: 1) Pressurization of the fuselage shell, which induces longitudinal and circumferential stresses that depend on the material properties and geometry, 2) Torsional loading of the fuselage shell, which causes shear stresses proportional to the applied torque and cross-sectional properties, and 3) Bending loads on wing spars, which are resisted by shear stresses in the spar webs and normal stresses in the spar caps that depend on the bending moment and section properties.
This document discusses analyzing stresses on an unsymmetrical tapered fuselage structure due to applied loads. It provides an example problem to determine stringer stresses and forces at two stations, section 0 and section 30, given loads applied at station 150. The solution strategy is outlined, which involves using the general bending stresses equation and calculating the centroid position with respect to the Z and Y axes. Steps are shown for calculating stresses at each section.
This document discusses material properties and bending stresses. It defines key terms like modulus of elasticity, Poisson's ratio, yield stress, and ultimate tensile stress. It explains that plane sections remain plane after bending but rotate, and that the neutral axis experiences no deformation or stress. The location of the neutral axis depends on the material properties and loading conditions. Equations are provided to calculate bending stresses based on the neutral axis location and applied moment. An example problem calculates bending stresses at different points on an airplanes wing. The document also notes that for very high loads above the elastic range, stresses become nonlinear and the neutral axis must be determined through trial and error.
The document outlines a lecture on fuselage structural design. It discusses iterative methods for calculating effective width and radius of gyration of thin-walled structures. It also covers loads acting on the fuselage, fuselage structure components like stringers and frames, and examples of analyzing stresses in circular fuselage sections. The document concludes by mentioning that stress analysis of wings will be covered next.
This document discusses effective sheet width and inter-rivet buckling in aerospace structures. It explains that stringers stiffen wing and fuselage skins, and skins provide stiffness to stringers even when buckling. An effective width calculation accounts for this effect. The document also describes how inter-rivet buckling can occur if rivet spacing is too long, and provides equations to calculate the effective rivet spacing to prevent this issue.
The document discusses the design of aircraft fuselages. It notes that fuselages must house passengers and luggage with proper strength and light weight. Fuselages experience both distributed and concentrated loads from various sources. A circular cross-section is commonly used as it efficiently handles these loads. Fuselage structures typically consist of a thin-walled tube with transverse frames, stringers, and cutouts. The document provides an example problem calculating the ultimate bending strength of a circular fuselage cross-section made of aluminum with stringers of different sizes. It considers linear and nonlinear stress distributions to determine the maximum moment the fuselage can withstand before failure.
- The fuselage skin consists of curved sheet panels that can buckle if no stiffeners are present. Stiffener elements are needed to calculate and compare the buckling loads to the aircraft's ultimate loads.
- Buckling of aircraft structures like fuselage skins must be analyzed and prevented. Curved sheets and cylinders can buckle under compression, bending, shear, torsion and combined loads. Internal pressure increases the buckling strength.
- Design examples are provided to calculate buckling loads of circular cylinders and curved-stiffened sheets under various loading conditions and determine if panels would buckle. Buckling analysis ensures the structure can withstand required loads.
1. The document discusses stresses in thin-walled and thick-walled cylinders. For thin-walled cylinders, the stress is assumed to be uniform throughout the wall. For thick-walled cylinders, the stresses depend on the radius and include circumferential (hoop), radial, and longitudinal stresses.
2. Internally pressurized thick-walled cylinders experience maximum hoop stress and compressive radial stress at the inner surface. The hoop stress decreases and radial stress increases towards zero at the outer surface. Longitudinal stress is uniform across the wall.
3. Externally pressurized thick-walled cylinders experience minimum hoop stress and compressive radial stress at the outer surface
This document provides an overview of various gear types and gear terminology. It discusses spur gears, helical gears, bevel gears, worm gears, and compares their basic configurations. Key gear concepts covered include involute tooth profiles, conjugate action, pressure angle, pitch circle, circular pitch, diametral pitch, addendum, dedendum, interference, contact ratio, and gear forming/cutting methods. Standard tooth systems and proportions are also presented in tables.
This document provides an overview of helical spring design and analysis. It discusses stresses in helical springs, deflection calculations, compression spring types, stability, materials selection, static design considerations, critical frequencies, and examples. The chapters cover key topics like curvature effects, stresses from torsion and shear, deflection-force relationships, buckling analysis, material properties, recommended design ranges, and the wave equation for vibrational frequency.
This document discusses threaded fasteners and screw threads. It defines common screw thread parameters like pitch, major diameter, and thread angle. It describes metric and unified screw thread standards. It also discusses power screws, different types of threaded fasteners, and how to select the proper fastener for an application based on required load and functional parameters.
The document discusses analyzing the stresses and deflections in aerospace shell beam structures like aircraft wings and space habitats. It presents an approach to idealize the cross-section into parts that carry extensional stress from bending and axial loads versus parts that carry shear stress from shear loads and torques. Joint equilibrium equations are developed and the problem is broken into "pure shear" and "pure torsion" cases that are then summed using superposition. Deflections are also analyzed by summing contributions from bending, shearing, and torsion.
The document discusses shear flow analysis of cantilevered wings. It presents equilibrium equations for 1-cell and 2-cell cantilevered wing models. Tables show shear flow analysis results for a 2-cell cantilevered wing with properties such as shear, bending moment, and torque calculated at each cell. Shear correction factors are also discussed.
This document outlines material properties testing methods and concepts. It discusses tensile testing to determine material strengths, stress-strain diagrams, elastic modulus, resilience, toughness, statistical variation in properties, effects of temperature and cold working. It also summarizes material classes including metals, plastics, composites and provides examples of common materials like steels, aluminum, titanium, polymers. Key material properties like strengths, moduli and factors affecting properties are defined.
This document discusses shaft design and layout. It covers selecting materials for shafts, including steel alloys. Geometric layout is discussed, including supporting axial loads and transmitting torque. Common shaft components like keys, pins, and set screws are described. Stress analysis equations for bending and torsion are provided. Estimating stress concentrations at features like shoulders is covered. The document contains many diagrams illustrating shaft configurations and components.
This document provides an overview of spring design and analysis. It discusses various types of springs including compression springs, extension springs, and torsion springs. It covers topics such as stresses in springs, deflection calculations, stability, materials selection, design considerations, fatigue loading, and critical frequencies. The document is presented in a series of slides intended for a lecture on spring design.
Literature Review Basics and Understanding Reference Management.pptxDr Ramhari Poudyal
Three-day training on academic research focuses on analytical tools at United Technical College, supported by the University Grant Commission, Nepal. 24-26 May 2024
Advanced control scheme of doubly fed induction generator for wind turbine us...IJECEIAES
This paper describes a speed control device for generating electrical energy on an electricity network based on the doubly fed induction generator (DFIG) used for wind power conversion systems. At first, a double-fed induction generator model was constructed. A control law is formulated to govern the flow of energy between the stator of a DFIG and the energy network using three types of controllers: proportional integral (PI), sliding mode controller (SMC) and second order sliding mode controller (SOSMC). Their different results in terms of power reference tracking, reaction to unexpected speed fluctuations, sensitivity to perturbations, and resilience against machine parameter alterations are compared. MATLAB/Simulink was used to conduct the simulations for the preceding study. Multiple simulations have shown very satisfying results, and the investigations demonstrate the efficacy and power-enhancing capabilities of the suggested control system.
Presentation of IEEE Slovenia CIS (Computational Intelligence Society) Chapte...University of Maribor
Slides from talk presenting:
Aleš Zamuda: Presentation of IEEE Slovenia CIS (Computational Intelligence Society) Chapter and Networking.
Presentation at IcETRAN 2024 session:
"Inter-Society Networking Panel GRSS/MTT-S/CIS
Panel Session: Promoting Connection and Cooperation"
IEEE Slovenia GRSS
IEEE Serbia and Montenegro MTT-S
IEEE Slovenia CIS
11TH INTERNATIONAL CONFERENCE ON ELECTRICAL, ELECTRONIC AND COMPUTING ENGINEERING
3-6 June 2024, Niš, Serbia
CHINA’S GEO-ECONOMIC OUTREACH IN CENTRAL ASIAN COUNTRIES AND FUTURE PROSPECTjpsjournal1
The rivalry between prominent international actors for dominance over Central Asia's hydrocarbon
reserves and the ancient silk trade route, along with China's diplomatic endeavours in the area, has been
referred to as the "New Great Game." This research centres on the power struggle, considering
geopolitical, geostrategic, and geoeconomic variables. Topics including trade, political hegemony, oil
politics, and conventional and nontraditional security are all explored and explained by the researcher.
Using Mackinder's Heartland, Spykman Rimland, and Hegemonic Stability theories, examines China's role
in Central Asia. This study adheres to the empirical epistemological method and has taken care of
objectivity. This study analyze primary and secondary research documents critically to elaborate role of
china’s geo economic outreach in central Asian countries and its future prospect. China is thriving in trade,
pipeline politics, and winning states, according to this study, thanks to important instruments like the
Shanghai Cooperation Organisation and the Belt and Road Economic Initiative. According to this study,
China is seeing significant success in commerce, pipeline politics, and gaining influence on other
governments. This success may be attributed to the effective utilisation of key tools such as the Shanghai
Cooperation Organisation and the Belt and Road Economic Initiative.
Embedded machine learning-based road conditions and driving behavior monitoringIJECEIAES
Car accident rates have increased in recent years, resulting in losses in human lives, properties, and other financial costs. An embedded machine learning-based system is developed to address this critical issue. The system can monitor road conditions, detect driving patterns, and identify aggressive driving behaviors. The system is based on neural networks trained on a comprehensive dataset of driving events, driving styles, and road conditions. The system effectively detects potential risks and helps mitigate the frequency and impact of accidents. The primary goal is to ensure the safety of drivers and vehicles. Collecting data involved gathering information on three key road events: normal street and normal drive, speed bumps, circular yellow speed bumps, and three aggressive driving actions: sudden start, sudden stop, and sudden entry. The gathered data is processed and analyzed using a machine learning system designed for limited power and memory devices. The developed system resulted in 91.9% accuracy, 93.6% precision, and 92% recall. The achieved inference time on an Arduino Nano 33 BLE Sense with a 32-bit CPU running at 64 MHz is 34 ms and requires 2.6 kB peak RAM and 139.9 kB program flash memory, making it suitable for resource-constrained embedded systems.
KuberTENes Birthday Bash Guadalajara - K8sGPT first impressionsVictor Morales
K8sGPT is a tool that analyzes and diagnoses Kubernetes clusters. This presentation was used to share the requirements and dependencies to deploy K8sGPT in a local environment.
Harnessing WebAssembly for Real-time Stateless Streaming PipelinesChristina Lin
Traditionally, dealing with real-time data pipelines has involved significant overhead, even for straightforward tasks like data transformation or masking. However, in this talk, we’ll venture into the dynamic realm of WebAssembly (WASM) and discover how it can revolutionize the creation of stateless streaming pipelines within a Kafka (Redpanda) broker. These pipelines are adept at managing low-latency, high-data-volume scenarios.
ACEP Magazine edition 4th launched on 05.06.2024Rahul
This document provides information about the third edition of the magazine "Sthapatya" published by the Association of Civil Engineers (Practicing) Aurangabad. It includes messages from current and past presidents of ACEP, memories and photos from past ACEP events, information on life time achievement awards given by ACEP, and a technical article on concrete maintenance, repairs and strengthening. The document highlights activities of ACEP and provides a technical educational article for members.
6th International Conference on Machine Learning & Applications (CMLA 2024)ClaraZara1
6th International Conference on Machine Learning & Applications (CMLA 2024) will provide an excellent international forum for sharing knowledge and results in theory, methodology and applications of on Machine Learning & Applications.