ahsanmehmood74

Aerospace Engineer

Jun 2024 - Present • 1 yr 11 mos

Design and Analysis for Kamikazes Drone System at Variable Conditions Design and Analysis of Loiter Munition System at Multiple Condition and Design Approach Using CFD Interceptor Design and Its Computational Study for Structure and Aerodynamics Electric V Tol System Design and Analysis for Variable Mission Regimes Civilian Specialized Drone Design and Analysis for Multiple Mission Constraints FPV Drone Design and Analysis for Optimization

Aerospace Engineering

Jan 2018 - Present • 8 yrs 4 mos

Worked as a conceptual and detailed design developer in the field of aviation and mechanical system using software like MATLAB, excel Worked in the department of optimization and innovation by the development of new and improved design related to the field of propulsion technology and general automotive and aerodynamic designs Worked as a structural analyst for the designing and improving of rotational mechanisms and structural systems Working as a freelancer for the past 28 month in the field of aviation technology and Mechanical Structures Worked as a propulsion analyst for two industrial clients working in the field of propulsion system designs and nozzle optimization by the use of CFD techniques Worked as a turbomachinery design engineer for several international client. Creation of turbines and Impellers were designed by the use of CFD and Turbomachinery software Worked on Ekranoplan Design and analysis by the use of various software for USA

Research Assistant for Propulsion and Power Engineering Lab

Dec 2023 - Jul 2024 • 7 mos

Thermal Analysis of a Combustion Chamber over Computational Fluid Mechanics Software using Internal Burning. Conjugate Heat Transfer Analysis using Internal Cooling System for a Combustion Chamber in Burning Conditions by CFD Software. Combustion Chamber Design for a Lower Altitude Missile System. Shear Injector Design for Liquid Propellent Rocket Engine. Injector CFD Analysis at Variable Liquid Propellent Mixture at Multiple Thermal Domain. Swirling Injector Design for mixing of Variable Rocket Propellants. Labyrinth Seal Design using Cryogenic Liquid for Rocket Boosters. Labyrinth Seal Analysis using CFD software for Cryogenic Fluids. Design and Analysis for a Cryogenic Pump System for an Industrial Gas Generator.