‪Debdoot Ghosh‬ - ‪Google Scholar‬

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2022202320241 1 2

Co-authors

Humrutha GunasekaranSimulation Analyst, Volvo India Pvt. Ltd.Verified email at volvo.com
Hideaki OgawaKyushu UniversityVerified email at aero.kyushu-u.ac.jp
Bibin JohnProfessor, VIT UniversityVerified email at vit.ac.in

Debdoot Ghosh

Debdoot Ghosh

Department of Aeronautics, Imperial College London

Verified email at vitstudent.ac.in - Homepage

High-Speed Aero-thermodynamics Supersonic Combustion CFD


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Large Eddy Simulation (LES) of Aerospike Nozzle Assisted Supersonic Retro-Propulsion (SRP) D Ghosh, H Gunasekaran AIAA Aviation 2021 Forum, 2489, 2021	4	2021
Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion (26th AIAA … D Ghosh, H Ogawa 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar …, 2022		2022
Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion D Ghosh, H Ogawa 26th AIAA Aerodynamic Decelerator Systems Technology Conference, 2734, 2022		2022
NUMERICAL INVESTIGATION OF OSCILLATING HYPERSONIC SHOCK WAVE BOUNDARY LAYER INTERACTIONS AT DIFFERENT FREQUENCIES D Ghosh, D Parthipan, B John

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Articles 1–4