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Finite Element Analysis
Mechanical Engineering
Python
Solidworks
Structural Engineering
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$15 USD / hour
Flag of PAKISTAN
multan, pakistan
$15 USD / hour
It's currently 8:27 AM here
Joined March 7, 2020
0 Recommendations

Muzaffar A.

@Muzaffar04

monthly-level-three.svg 5.0 (1 review)
1.3
1.3
100%
100%
$15 USD / hour
Flag of PAKISTAN
multan, pakistan
$15 USD / hour
100%
Jobs Completed
100%
On Budget
100%
On Time
N/A
Repeat Hire Rate

Aerospace, Drone/UAV, CFD/FEA, SolidWorks, Design

As an Aerospace Engineer with 4+ years of industry experience, I have expertise in Ansys simulations and product design optimization. With a demonstrated history of success, I excel in designing, researching, and developing a wide range of mechanical structures and products. From mechanical components to cutting-edge advancements such as Drones, Aircraft and Defence products, and Missile Systems, I have executed diverse projects with exceptional precision and efficiency. My passion for innovation and strong problem-solving abilities have been key drivers behind my accomplishments in this field. Computational Fluid Dynamics (CFD) In my Computational Fluid Dynamics (CFD) work, I specialize in optimizing airflow around drones, UAVs (unmanned aerial vehicles), and aircraft to enhance their efficiency and performance. Utilizing Ansys Fluent and CFX, I simulate complex air dynamics to design vehicles that are faster, safer, and more fuel-efficient. My focus extends to reducing drag, improving lift, and ensuring quiet operation, addressing aerodynamic challenges across various flight conditions. Aero Vehicle Design: In Aero Vehicle Design, my expertise is adeptly applied to the development of high-performance air vehicles, including UAVs, drones, and traditional aircraft, from conceptual design to detailed aerodynamic analysis. By leveraging Roskam Advanced Aircraft Analysis (AAA) and Raymer Design Software (RDS), I specialize in engineering optimized designs for UAVs, drones, and aircraft that adhere to the strictest aerospace standards. My capability extends to employing XFLR5 for the aerodynamic performance assessment of UAVs and drones, alongside JAVA Foil for precise airfoil analysis. I am proficient in 3D printing technologies for rapid prototyping of 3D printed Drones and UAVs including both rotary and fixed wings. I significantly expedite the design iteration process for UAVs, drones, and aircraft, ensuring swift progress from concept to reality. Finite Element Analysis (FEA) In my Finite Element Analysis (FEA) practice, I focus on enhancing the structural integrity and resilience of a wide range of projects, from drones and aircraft to vehicle frames and mechanical components. I have great command over the following Software Skills: • Ansys (Fluent, CFX, ICEM, Static Structural Analysis, etc) • COMSOL • Abaqus • SolidWorks • CATIA • AutoCad • Matlab • Simulink • Advanced Aircraft Analysis (AAA) • Raymer Design Software (RDS) • JAVA Foil • XFLR5 I am dedicated to delivering high-quality work within deadlines, with a strong emphasis on client satisfaction and building long-term relationships. Using my expertise, I aim to provide solutions that precisely meet your goals. You can rely on me to deliver the perfect solution to accomplish your objectives. Thank you for taking the time to explore my profile. Please feel free to reach out to me at any time for work or consultation.
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Portfolio

11870596
Embark on a cutting-edge journey through my expertise in aerial detection and tracking of vehicles and pedestrians, leveraging the power of YOLOv8 and DCF trackerEmbark on a cutting-edge journey through my expertise in aerial detection and tracking of vehicles and pedestrians, leveraging the power of YOLOv8 and DCF tracker. In this project, I seamlessly integrate these advanced technologies to create a robust and efficient solution. The pinnacle of the project lies in the deployment of a fully automated pipeline on the Jetson Nano platform, utilizing Nvidia Deepstream for real-time processing.
Aerial Surveillance Automation with YOLOv8
11870586
In this project, Structural and modal analyses of Engine Mount of MFI-17/Mushshak Aircraft was performed. It was designed for installation of SAFRAN SMA SR305-230E engine. Structural loads were calculated under 4.4 g, 1g and -2g loading conditions and were applied on engine centre of gravity. Factor of safety, Von Mises stress and Maximum deformation of the engine mount for three load cases were calculated for results. Lowest value of factor of safety under extreme loading condition found was 1.87, ensuring that the engine mount is safe.
Aircraft Engine Mount Structural (FEA) Analysis
In this project, Structural and modal analyses of Engine Mount of MFI-17/Mushshak Aircraft was performed. It was designed for installation of SAFRAN SMA SR305-230E engine. Structural loads were calculated under 4.4 g, 1g and -2g loading conditions and were applied on engine centre of gravity. Factor of safety, Von Mises stress and Maximum deformation of the engine mount for three load cases were calculated for results. Lowest value of factor of safety under extreme loading condition found was 1.87, ensuring that the engine mount is safe.
Aircraft Engine Mount Structural (FEA) Analysis
11870583
In this project, I designed and simulated an advanced supersonic tail-controlled missile. Using ANSYS Fluent, I analyzed its aerodynamics both at rest and in motion. By calculating various aerodynamic coefficients, I gained crucial insights into its flight behavior. With this data, I developed a sophisticated flight controller that enhances the missile's maneuverability and accuracy. This project explores the exciting world of high-speed missiles, combining theory and practice to create a cutting-edge weapon system.
Design & CFD analysis of Supersonic Tail-controlled Missile
In this project, I designed and simulated an advanced supersonic tail-controlled missile. Using ANSYS Fluent, I analyzed its aerodynamics both at rest and in motion. By calculating various aerodynamic coefficients, I gained crucial insights into its flight behavior. With this data, I developed a sophisticated flight controller that enhances the missile's maneuverability and accuracy. This project explores the exciting world of high-speed missiles, combining theory and practice to create a cutting-edge weapon system.
Design & CFD analysis of Supersonic Tail-controlled Missile
11198823
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
11198819
In this project, I conducted a Computational Fluid Dynamics (CFD) analysis of a Formula One Car using ANSYS. The CFD analysis allows to evaluate critical factors such as downforce, drag, and flow patterns around the car's surfaces, leading to optimized designs for enhanced speed and stability on the track.
CFD Analysis of a Formula One Car
In this project, I conducted a Computational Fluid Dynamics (CFD) analysis of a Formula One Car using ANSYS. The CFD analysis allows to evaluate critical factors such as downforce, drag, and flow patterns around the car's surfaces, leading to optimized designs for enhanced speed and stability on the track.
CFD Analysis of a Formula One Car
11198817
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump
11870596
Embark on a cutting-edge journey through my expertise in aerial detection and tracking of vehicles and pedestrians, leveraging the power of YOLOv8 and DCF trackerEmbark on a cutting-edge journey through my expertise in aerial detection and tracking of vehicles and pedestrians, leveraging the power of YOLOv8 and DCF tracker. In this project, I seamlessly integrate these advanced technologies to create a robust and efficient solution. The pinnacle of the project lies in the deployment of a fully automated pipeline on the Jetson Nano platform, utilizing Nvidia Deepstream for real-time processing.
Aerial Surveillance Automation with YOLOv8
11870586
In this project, Structural and modal analyses of Engine Mount of MFI-17/Mushshak Aircraft was performed. It was designed for installation of SAFRAN SMA SR305-230E engine. Structural loads were calculated under 4.4 g, 1g and -2g loading conditions and were applied on engine centre of gravity. Factor of safety, Von Mises stress and Maximum deformation of the engine mount for three load cases were calculated for results. Lowest value of factor of safety under extreme loading condition found was 1.87, ensuring that the engine mount is safe.
Aircraft Engine Mount Structural (FEA) Analysis
In this project, Structural and modal analyses of Engine Mount of MFI-17/Mushshak Aircraft was performed. It was designed for installation of SAFRAN SMA SR305-230E engine. Structural loads were calculated under 4.4 g, 1g and -2g loading conditions and were applied on engine centre of gravity. Factor of safety, Von Mises stress and Maximum deformation of the engine mount for three load cases were calculated for results. Lowest value of factor of safety under extreme loading condition found was 1.87, ensuring that the engine mount is safe.
Aircraft Engine Mount Structural (FEA) Analysis
11870583
In this project, I designed and simulated an advanced supersonic tail-controlled missile. Using ANSYS Fluent, I analyzed its aerodynamics both at rest and in motion. By calculating various aerodynamic coefficients, I gained crucial insights into its flight behavior. With this data, I developed a sophisticated flight controller that enhances the missile's maneuverability and accuracy. This project explores the exciting world of high-speed missiles, combining theory and practice to create a cutting-edge weapon system.
Design & CFD analysis of Supersonic Tail-controlled Missile
In this project, I designed and simulated an advanced supersonic tail-controlled missile. Using ANSYS Fluent, I analyzed its aerodynamics both at rest and in motion. By calculating various aerodynamic coefficients, I gained crucial insights into its flight behavior. With this data, I developed a sophisticated flight controller that enhances the missile's maneuverability and accuracy. This project explores the exciting world of high-speed missiles, combining theory and practice to create a cutting-edge weapon system.
Design & CFD analysis of Supersonic Tail-controlled Missile
11198823
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
In this project, I undertook the design and simulation of a trainer Unmanned Aerial Vehicle (UAV) with the added dimension of flight gear visualization. Employing ANSYS Fluent, I conducted comprehensive static and dynamic Computational Fluid Dynamics (CFD) analysis, allowing me to precisely assess its aerodynamics during various flight scenarios. By calculating essential aerodynamic coefficients, I gained valuable insights into the UAV's performance characteristics. Utilizing this aerodata, I successfully developed an advanced flight controller that significantly enhances the UAV's maneuverability and stability. The integration of flight gear visualization further enriched the project.
Design and CFD Analysis of a trainer Unmanned Aerial Vehicle
11198819
In this project, I conducted a Computational Fluid Dynamics (CFD) analysis of a Formula One Car using ANSYS. The CFD analysis allows to evaluate critical factors such as downforce, drag, and flow patterns around the car's surfaces, leading to optimized designs for enhanced speed and stability on the track.
CFD Analysis of a Formula One Car
In this project, I conducted a Computational Fluid Dynamics (CFD) analysis of a Formula One Car using ANSYS. The CFD analysis allows to evaluate critical factors such as downforce, drag, and flow patterns around the car's surfaces, leading to optimized designs for enhanced speed and stability on the track.
CFD Analysis of a Formula One Car
11198817
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump
In this turbomachinery project, we embarked on the Design and Simulation of an innovative Electric Cryogenic Fuel Pump, aimed at achieving a pressure head of 60 bar. Leveraging the powerful tools CF_Turbo, we meticulously crafted the pump's intricate design, ensuring optimal efficiency and performance. Through extensive simulations using CFX, we scrutinized the pump's behavior under various operating conditions, gaining valuable insights into its fluid dynamics and thermal characteristics. With a focus on cryogenic fuel handling, our pump's design aims to meet the demanding requirements of high-pressure applications, paving the way for enhanced propulsion systems in space exploration and beyond. To materialize our design, we crafted the manufacturing Computer-Aided Design (CAD) using Solidworks, ensuring precision and accuracy in the production process.
Design and Simulation of an Electric Cryogenic Fuel Pump

Reviews

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5.0
$45.00 USD
UAV Structural Improvement via FEA
I am extremely pleased with the UAV structural improvement project carried out by Muzaffar Ahmed. His expertise in Finite Element Analysis (FEA) was evident throughout the process. He demonstrated a deep understanding of UAV dynamics and effectively implemented improvements, enhancing overall structural integrity. The attention to detail and timely delivery exceeded my expectations. I highly recommend Muzaffar Ahmed for any FEA-related projects.
Engineering
Solidworks
Mechanical Engineering
Structural Engineering
Finite Element Analysis
A
Flag of Abdullah A.
@Abosalah123
•
4 months ago

Experience

Design Engineer

Inphoenix Aviation Pvt. Ltd.
Dec 2022 - Present
As a design engineer at Inphoenix Aviation Pvt Ltd., my main job duties include tasks related to CAD modeling, UAV design, and CFD simulations for various aircraft. I am responsible for creating detailed and precise CAD models, contributing to the design of Unmanned Aerial Vehicles (UAVs), and conducting CFD simulations to analyze the aerodynamics and performance of different aircraft.

Aerospace Design Engineer

Aviation Engineering Solutions Pvt. Ltd.
Sep 2019 - Nov 2022 (3 years, 2 months)
During my time at Aviation Engineering Solutions Pvt Ltd, I have designed various 3D models for aircraft components, with a specific focus on the Air Conditioning System and Electric Trim System of Super Mushshak Aircraft. Additionally, I have been involved in the Civil Certification process, collaborating closely with the Pakistan Civil Aviation Authority to ensure the compliance and safety of various aviation components.

Education

MS Aerospace Engineering

Institute of Space Technology , Pakistan 2019 - 2023
(4 years)

BS Aerospace Engineering

Institute of Space Technology , Pakistan 2015 - 2019
(4 years)

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Top Skills

Solidworks 1
Mechanical Engineering 1
Structural Engineering 1
Finite Element Analysis 1
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