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Title of Article

STUDYING THE PERFORMANCE OF THE SCRAMJET MODEL IN A HYPERSONIC PULSE WIND TUNNEL


Issue
4
Date
 2011

Article type
 scientific article
UDC
533.6;53.082.5
Pages
673-674
Keywords
 


Authors
Vasilev I.Yu.
Institut prikladnoy mekhaniki RAN, Moskva

Zakharov N.N.
Institut prikladnoy mekhaniki RAN, Moskva

Polyanskikh A.V.
Institut prikladnoy mekhaniki RAN, Moskva

Prudnikov A.G.
Tsentralnyy institut aviatsionnogo motorostroeniya im. P.I. Baranova, Moskva


Abstract
Some problems mainly related to the interaction of supersonic and hypersonic jets and the surface of a flying vehicle are considered. The results of the experimental study in the IPRIM RAS Hypersonic Pulse Wind Tunnel at Mach number M=2? 7 are presented.

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