DERIVATION BY A TRANSFORM METHOD OF INTEGRAL EQUATIONS OF UNSTEADY LIFTING SURFACE THEORY IN SUBSONIC AND SUPERSONIC FLOW.

被引：0

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作者：

Ando, Shigenori

Ichikawa, Akio

机构：

来源：

Aeronautical Quarterly | 1979年 / 30卷 / pt 4期

关键词：

Compendex;

D O I：

10.1017/s0001925900008714

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学科分类号：

摘要：

Aerodynamics

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页码：529 / 543

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[1] DERIVATION BY A TRANSFORM METHOD OF INTEGRAL-EQUATIONS OF UNSTEADY LIFTING SURFACE THEORY IN SUBSONIC AND SUPERSONIC-FLOW
ANDO, S
ICHIKAWA, A
AERONAUTICAL QUARTERLY, 1979, 30 (NOV): : 529 - 543
[2] Continuity of lifting surface theory in subsonic and supersonic flow
Ueda, T
AIAA JOURNAL, 1998, 36 (10) : 1788 - 1791
[3] CALCULATING KERNEL OF LIFTING SURFACE INTEGRAL EQUATION IN UNSTEADY SUBSONIC FLOW
DAT, R
MALFOIS, JP
RECHERCHE AEROSPATIALE, 1970, (05): : 251 - &
[4] APPLICATION OF LIFTING LINE THEORY TO STREAMSURFACE THEORY IN SUBSONIC FLOW.
CHANG, P.T.
1600, (V 104):
[5] UNSTEADY LIFTING SURFACE THEORY FOR SUPERSONIC THROUGH-FLOW FAN
NAMBA, M
HANADA, T
JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 1994, 37 (04): : 760 - 768
[6] Integral Method for Uniform Calculation of Subsonic and Supersonic Regions in a Plane and Axisymmetrical Hypersonic Flow.
Baston, Alfred
1600, (20):
[7] A GENERAL METHOD FOR SOLVING PROBLEMS OF THE UNSTEADY LIFTING SURFACE THEORY IN THE SUBSONIC RANGE
KUESSNER, HG
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (01): : 17 - &
[8] APPLICATION TO ROTARY WINGS OF A SIMPLIFIED AERODYNAMIC LIFTING SURFACE THEORY FOR UNSTEADY COMPRESSIBLE FLOW.
Rao, B.M.
Jones, W.P.
1974,
[9] A NOTE ON SUPERSONIC WING INTEGRAL EQUATIONS IN UNSTEADY FLOW
MILES, JW
AERONAUTICAL QUARTERLY, 1952, 3 (04): : 294 - 296
[10] ALTERNATIVE SOLUTION OF THE KERNEL FUNCTION IN SUBSONIC UNSTEADY LIFTING SURFACE THEORY
EPSTEIN, RJ
BLISS, DB
AIAA JOURNAL, 1995, 33 (11) : 2228 - 2230

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