Aerodynamic Characterization of Hypersonic Launch Vehicle laden with exposed Scramjet based Cruise Vehicle-Reference-Cited by-同舟云学术

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Aerodynamic Characterization of Hypersonic Launch Vehicle laden with exposed Scramjet based Cruise Vehicle

Published:2023-05-27 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Mahato Mrinal¹,Sarikonda Srinivasa Raju¹,Balasubramanian R¹,K Anadhanarayanan¹,T K Ganesh Anavaradham¹,Chattopadhayay Sandip¹

Affiliation:

1. DRDL

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3035

Reference4 articles.

1. Tip-to-tail numerical simulation of a hypersonic air-breathing engine with ethylene fuel

2. Computational Fluid Dynamics Simulation of Tip-to-Tail for Hypersonic Test Vehicle

3. Sarwade, A.G., Narayana, A.S., Ganesh Anavaradham, T.K., Patil, S.R. and Panneerselvam, S. "Theoretical and experimental studies on a semi-ellipsoid body with airframe components", AIAA 2002-5223.

4. STAR-CCM+Documentation,Version12.02,2017PLMSoftware Inc.www.siemens.com/mdx.

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