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Supersonic flow around a body of small elongation
Authors:S. V. Guvernyuk  A. F. Zubkov  K. M. Pichkhadze  V. S. Finchenko  A. I. Shvets
Affiliation:1. Faculty of Mechanics and Mathematics, Moscow State University, Leninskie Gory, Moscow, 119899, Russia
Abstract:Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.
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