Drag reduction for the combination of spike and counterflow jet on blunt body at high Mach number flow-Reference-Cited by-同舟云学术

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Drag reduction for the combination of spike and counterflow jet on blunt body at high Mach number flow

Published:2017-04 Issue: Volume:133 Page:103-110
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Eghlima Z.,Mansour K.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. The flow of a jet from a body opposing a supersonic free stream;Finley;J. Fluid Mech.,1966

2. D.H. Crawford, Investigation of flow over a spiked nose hemisphere-cylinder at Mach number of 6.8 NASA-TN-D-118, 1959.

3. Preliminary investigations of spiked bodies at hypersonic speeds;Bogdonoff;J. Aerosp. Sci.,1959

4. An experimental investigation of stagnation-point injection;Barber;J. Spacecr. Rockets,1965

5. Flow oscillations of spike-tipped bodies;Shang;AIAA J.,1982

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