HYPERSONIC SIMILARITY AND THE TANGENT-CONE APPROXIMATION FOR UNYAWED BODIES OF REVOLUTION

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作者：

PROBSTEIN, RF

BRAY, KNC

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JOURNAL OF THE AERONAUTICAL SCIENCES | 1955年 / 22卷 / 01期

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V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：66 / 68

页数：3

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[21] INVESTIGATIONS ON HYPERSONIC FLOW PAST BLUNT BODIES OF REVOLUTION WITH NOSEBLOWING
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[27] SIMILARITY LAWS FOR BODIES MAXIMIZING LIFT-TO-DRAG RATIO AT HYPERSONIC SPEEDS
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[28] Investigation of aerodynamic characteristics of a hypersonic flow around bodies of revolution with a permeable tip
Sidnyaev, N. I.
[J]. JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2007, 48 (02) : 159 - 165
[29] LIMITING HYPERSONIC FLOW NEAR THE STAGNATION POINT OF BODIES OF REVOLUTION AT ANGLE OF ATTACK
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[J]. CONTINUUM MECHANICS AND ITS APPLICATIONS, 1989, : 667 - 678
[30] Investigation of aerodynamic characteristics of a hypersonic flow around bodies of revolution with a permeable tip
N. I. Sidnyaev
[J]. Journal of Applied Mechanics and Technical Physics, 2007, 48 : 159 - 165

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