Spike root oblique jet effect on drag and heat load reduction performance for hypersonic vehicles
Author:
Funder
Fundamental Research Funds for the Central Universities
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference54 articles.
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3. Numerical investigation of a spiked blunt nose cone at hypersonic speeds;Gauer;J. Spacecraft Rockets,2008
4. Drag reduction using aerodisks for hypersonic hemispherical bodies;Ahmed;J. Spacecraft Rockets,2010
5. Assessment of the aerodisk size on drag reduction and thermal protection of high-bluntness vehicles at hypersonic speeds;Kharati-Koopaee;J. Aero. Eng.,2017
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