LINEARIZED THEORY OF PLANE, UNSTEADY, SUPERSONIC-FLOW THROUGH ACASCADE (SUBSONIC LEADING EDGES LOCUS)

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作者：

SALAUN, P

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RECHERCHE AEROSPATIALE | 1978年 / 03期

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V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：125 / 132

页数：8

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[1] ON A LINEAR-THEORY OF A SUPERSONIC-FLOW PAST A DELTA WING WITH SUBSONIC LEADING EDGES
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[2] SUCCESSIVE APPROXIMATIONS OF CALCULATION OF SUPERSONIC-FLOW CONCERNING FLIGHT WITH SUBSONIC LEADING EDGES
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[3] A NOTE ON SUBSONIC EDGES IN UNSTEADY SUPERSONIC FLOW
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QUARTERLY OF APPLIED MATHEMATICS, 1953, 11 (03) : 363 - 367
[4] UNSTEADY-FLOW IN A SUPERSONIC CASCADE WITH SUBSONIC LEADING-EDGE LOCUS
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[5] DERIVATION BY A TRANSFORM METHOD OF INTEGRAL-EQUATIONS OF UNSTEADY LIFTING SURFACE THEORY IN SUBSONIC AND SUPERSONIC-FLOW
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[6] LINEARIZED SOLUTIONS FOR THE SUPERSONIC-FLOW THROUGH TURBOMACHINERY BLADE ROWS (USING ACTUATOR DISK THEORY)
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[7] AERODYNAMIC APPROXIMATIONS FOR UNSTEADY SUPERSONIC-FLOW THROUGH DUCTS OF REVOLUTION
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[8] NEIGHBORHOOD OF THE LEADING-EDGE OF A PLANE POINTED PROFILE IN SUPERSONIC-FLOW
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PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1979, 43 (03): : 517 - 526
[9] LINEARIZED THEORY OF SUBSONIC UNSTEADY FLOW IN A 2-DIMENSIONAL STRAIGHT CASCADE
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[10] EQUATION SYSTEMS FOR THE INDIRECT PROBLEM OF STEADY SUBSONIC AND SUPERSONIC-FLOW THROUGH TURBOMACHINES, INCLUDING LOSSES AND HEAT-FLOW
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FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 1981, 47 (02): : 62 - 66