Implementation of concavity over heat shield of a reentry vehicle in reducing aerodynamic heating-Reference-Cited by-同舟云学术

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Implementation of concavity over heat shield of a reentry vehicle in reducing aerodynamic heating

Published:2024-07 Issue: Volume:107 Page:109413
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Sai Naga Bharghava Dorbala,Krishnat Mali Amit,Jana Tamal,Kaushik Mrinal^ORCID

Publisher

Elsevier BV

Reference37 articles.

1. Recent advances in the aerothermodynamics of spiked hypersonic vehicles;Ahmed;Prog. Aerosp. Sci.,2011

2. Aerothermal Testing for Project Orion Crew Exploration;Berry,2009

3. Strategies to utilize advanced heat shield technology for high-payload Mars atmospheric entry missions;Braun;Acta Astronaut.,2017

4. Effect of Counterflow Jet on a Supersonic Reentry Capsule;Chang,2006

5. Aerodynamic design of a re-entry capsule for high-speed manned re-entry;Chen;Acta Astronaut.,2015

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