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ICMARACTUAL AEROGASDYNAMIC PROBLEMS OF HIGH SUPERSONIC INLETS Yu.P. Gounko Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
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Document Date: 2014-12-04 04:51:53


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City

Manchester / Moscow / Kazan / Lyon / Novosibirsk / Marseille / /

Company

Acs / Rudakov A.S. / /

Country

France / Russia / United States / United Kingdom / /

Facility

Keldysh Research Center / Gounko Khristianovich Institute of Theoretical / NASA Langley Research Center / /

IndustryTerm

supersonic aircraft carrier / oil-film / aircraft carrier / Oil-film patterns / aerospace plane / internal gas flows / aerospace craft / machinery / aerospace planes / gas dynamics / oil-film visualized flow patterns / aerospace system / /

NaturalFeature

Adjusted Inlet / Convergent inlet / /

Organization

Gounko Khristianovich Institute of Theoretical / Keldysh Research Center / Russian Academy of Sciences / Mikoyan Design Bureau / Tupolev Design Bureau / National Aeronautics and Space Administration / NASA Langley Research Center / Scientific Research Institute / NASA CR / /

Person

Van Wie / V.A. Skibin / V / /

Position

Lukashevitch V.P. / Representative / /

Product

Tu-2000 / lifting body / Skullcandy G.I. Headphone/Headset / X-43A / /

Technology

aero / 3G / flash / /

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