The drag reduction in spherical spiked blunt body
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference21 articles.
1. D.H. Crawford. Investigation of the Flow Over a Spiked-nose Hemisphere-cylinder at Mach Number 6.8, Jones, R.Z. NASA TN D-118., Washington, December 1959.
2. Preliminary investigation of spiked bodies at hypersonic speeds;Bogdonoff;J. Aerosp. Sci.,1959
3. Drag on blunt bodies with and without spikes in low-density hypersonic flow;Sims;AIAA,1965
4. Influence of spike shape at supersonic flow past blunt-nosed bodies;Milichev;AIAA,2002
5. Numerical investigation of supersonic flows around a spiked blunt body;Yamauchi;J. Spacecraft Rockets,1995
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