Hypersonic drag and heat reduction mechanism of a new hybrid method of spike, multi-row discs and opposing jets aerodynamic configuration
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference54 articles.
1. Preliminary investigations of spiked bodies at hypersonic speeds;Bogdonoff;J. Aerosp. Sci.,1959
2. Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach number;Viren;Shock Waves,2002
3. Aerodynamic spike flowfields computed to select optimum configuration at Mach 2.5 with experimental validation;Shoemaker,1990
4. Numerical investigation of a spiked blunt nose cone at hypersonic speeds;Gauer;J. Spacecr. Rocket.,2008
5. Unsteady aerodynamic considerations in the design of a drag-reduction spike;Reding;J. Spacecr. Rocket.,1977
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