Numerical modelling of supersonic inviscid gas flow around lifting configurations
V.F. Volkov, A.A. Zheltovodov, M.S. Loginov
Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
Pages: 205-220
Abstract
The results of numerical computations are presented for three-dimensional supersonic flow around the lifting elements of flying vehicles on the basis of the Euler equations. The flow around different configurations of the lifting body of the ELAC 1 type (M∞ = 2.02; 4.04, -3
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