Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows
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Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-540-85168-4_90.pdf
Reference8 articles.
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2. Balla Venukumar, G. Jagadeesh and K.P.J. Reddy,: Counterflow drag reduction by a supersonic jet for a blunt body in hypersonic flow, Physics of fluids, 18, 118104 (2006)
3. V. Menezes, S. Kumar, Maruta, K. P. J. Reddy, and K. Takayama,: Hypersonic flow over a multi-step afterbody, Shock Waves Vol. 14, pp 421-424, (2005).
4. Viren M, Saravanan S, Reddy KPJ, : Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach number, Shock Waves Vol 12, pp 197-204 (2002)
5. Gnemmi, P., Srulijes, J., Roussel, K., and Runne, K. : Flow Field around Spike-Tipped Bodies, AIAA Paper 2001-2464, June 2001.
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