Wind-tunnel tests of a model scramjet under high Mach and Reynolds numbers
Yu.P. Goonko, V.I. Zvegintsev, I.I. Mazhul, D.G. Nalivaichenko, I.S. Turko, A.M. Kharitonov, and V.F. Chirkashenko
Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
Pages: 315–338
Abstract
The paper describes results on testing a model scramjet with a three-dimensional inlet in the new adiabatic-compression wind tunnel AT 303 recently put into operation at the Institute of Theoretical and Applied Mechanics, SB RAS. The wind tunnel operates, covering the range of free-stream Mach numbers M  |
