Development of maximum conical shock angle limit for osculating cone waveriders-Reference-Cited by-同舟云学术

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Development of maximum conical shock angle limit for osculating cone waveriders

Published:2024-04 Issue: Volume:147 Page:109031
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ghosh Agnivo^ORCID,Rao Srisha M.V.^ORCID

Publisher

Elsevier BV

Reference50 articles.

1. Hypersonic and High-Temperature Gas Dynamics;Anderson,2019

2. Hypersonic Aerothermodynamics;Bertin,1994

3. Aerothermal testing for project Orion crew exploration vehicle;Berry,2009

4. ESA ExoMars program: the next step in exploring Mars;Vago;Sol. Syst. Res.,2015

5. Novel approach for designing a hypersonic gliding–cruising dual waverider vehicle;Liu;Acta Astronaut.,2014

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic and Stability Analyses of Osculating Cone Waveriders with Variable Tip Shapes;2024

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