Srujan Kumar Email & Phone Number

London Area, United Kingdom

Reviewed feasible propellant systems for sub 200 kg small satellite.• Shortlisted propellants after trade off studies and within constrains in designrequirements.• Preliminary estimation of propellant masses for different propellent and mission profiles.

Cranfield University

• Executed a comprehensive steady and unsteady CFD analysis of a wind tunnel test section featuring an aero engine cowl cross section.• Evaluated the influence of Mass flow capture ratio on flow characteristics across the cowl, concentrating on the provocation of shock-induced separation.• Contrasted and analysed outcomes derived from different turbulence models (Kw-SST & SA) and examined the impact of intermittency (TSST) on wall shear stress to appraise separation.• Confirmed the absence of wall-related effects on the probe measurement plane by conducting 3D unsteady simulations under varying windmilling conditions.• Mastered the automation of simulations through journal file scripting, skilfully performed post-processing using Python and Paraview.• Preparation of technical reports, Applying acquired skills,

Greater Hyderabad Area

Performed a comprehensive technical review of secondary injection thrust vectoring.Participated in an immersive orientation program focusing on the design and development of missile systems, with a specific emphasis on liquid propulsion systems and structural testing of diverse airframe sections for missile applications.Gained proficiency in the design and development of thrust vectoring systems tailored for booster stages.

India

Used 3D CAD modelling tools for to design and improve systems meeting FAA standards and also successfully performed structural analysis of wing, body and landing gear.• Conducted a deep evaluation of conceptual design including mission requirements, configuration, and performance characteristics, Delivering technical assignments, Preparation of technical reports, Design development, Design Calculations.• Created drawings, instructions, specifications & documentation on equipment, devices

Master'S Degree, Aerospace Propulsion, A

M.Sc. Thermal Power - Aerospace Propulsion Cranfield University, United Kingdom Modules: Gas turbine Performance Simulation.

Bachelors, Aeronautical/Aerospace Engineering Technology/Technician, Distinction

B.Tech. Aerospace engineering Hindustan Institute of Technology and Science, India Modules: Aerodynamics, Propulsion, Gas dynamics, Heat.

Aerospace, Aeronautical And Astronautical Engineering, A

Design and computational fluid dynamics analysis of a Medium haul commercial aircraft wing and fuselage”, IJITEE, Volume-8 Issue-10, Page.