Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s12046-007-0011-0.pdf
Reference11 articles.
1. Balla Venukumar, Jagadeesh G, Reddy K P J 2006 Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow. Phys. Fluids 18: Art. No. 118104
2. Josyula E, Pinney M, Blake W M 2001 Application of a counterflow drag reduction technique in high speed systems. AIAA Paper 01-2437.
3. Hayashi K, Asoy S 2003 Effect of pressure ratio on aerodynamic heating reduction due to opposing jet. AIAA Paper 03-4041
4. Menezes V, Saravanan S, Jagadeesh G, Reddy K P J 2003 Experimental investigations of hypersonic flow over highly blunted cones with aerospikes. AIAA J. 41: 1955–1966
5. Menezes V, Kumar S, Maruta K, Reddy K P J, Takayama K 2005 Hypersonic flow over a multi-step afterbody, Shock Waves 14: 421–424
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