ANALYTICAL COMPARISON OF HYPERSONIC FLIGHT AND WIND TUNNEL VISCOUS/INVISCID FLOW FIELDS.

被引：0

作者：

Fivel, H.J.

Masek, R.V.

Mockapetris, L.J.

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来源：

| 1600年

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Compendex;

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摘要：

FLOW OF FLUIDS

引用

共 6 条

[1] Wind Tunnel Measurements of a Model in Rarefied Hypersonic Flow.
Buetefisch, K.A.
Schoeler, H.
Raumfahrtforschung, 1974, 18 (01): : 10 - 16
[2] Analytical Upwash Approximations of Generalized Conical Supersonic Flow Fields.
Leiter, Erich
Zeitschrift fuer Flugwissenschaften, 1975, 23 (03): : 69 - 76
[3] EFFECT OF THE RELATIVE AREA OF THE FLOW CORE ON THE PERFORMANCE OF A HYPERSONIC WIND TUNNEL.
Bezmenov, V.Ya.
Fluid mechanics. Soviet research, 1979, 8 (01): : 122 - 132
[4] Comparison of Ares I-X Flight and Wind-Tunnel Aeroacoustic Data
Reed, Darren K.
Mayle, Melody N.
Nance, Donald K.
JOURNAL OF SPACECRAFT AND ROCKETS, 2012, 49 (04) : 659 - 665
[5] Measurement of Flow Fields by Laser-Doppler Technique in a Supersonic Wind Tunnel.
Maurer, F.
Petersen, J.C.
Pfeifer, H.J.
Haertig, J.
Bundesministerium fuer Forschung und Technologie, Forschungsbericht; Weltraumforschung, 1975, (75-15):
[6] PRELIMINARY COMPARISON BETWEEN THE SR-3 PROPELLER NOISE IN FLIGHT AND IN A WIND TUNNEL.
DITTMAR, JAMES H.
LASAGNA, PAUL L.
1982,