ON A LINEAR-THEORY OF A SUPERSONIC-FLOW PAST A DELTA WING WITH SUBSONIC LEADING EDGES

被引：0

|

作者：

KUBO, S

机构：

来源：

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 1980年 / 23卷 / 61期

关键词：

Compendex;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

AERODYNAMICS

引用

收藏

页码：127 / 138

页数：12

相关论文

共 50 条

[1] FLOW PAST DELTA-WING-HALF-CONE COMBINATION WITH SUBSONIC LEADING EDGES
PORTNOY, H
AERONAUTICAL QUARTERLY, 1964, 15 (04): : 311 - &
[2] LINEARIZED THEORY OF PLANE, UNSTEADY, SUPERSONIC-FLOW THROUGH ACASCADE (SUBSONIC LEADING EDGES LOCUS)
SALAUN, P
RECHERCHE AEROSPATIALE, 1978, (03): : 125 - 132
[3] SUCCESSIVE APPROXIMATIONS OF CALCULATION OF SUPERSONIC-FLOW CONCERNING FLIGHT WITH SUBSONIC LEADING EDGES
LEITER, E
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1973, 53 (05): : 247 - 259
[4] Linear Approximation for Supersonic Flow Past a Delta Wing
Shuxing Chen
Archive for Rational Mechanics and Analysis, 1997, 140 : 319 - 333
[5] Linear approximation for supersonic flow past a delta wing
Chen, SX
ARCHIVE FOR RATIONAL MECHANICS AND ANALYSIS, 1997, 140 (04) : 319 - 333
[6] Linear approximation for supersonic flow past a delta wing
Institute of Mathematics, Fudan University, Shanghai, 200433, China
Arch Ration Mech Anal, 4 (319-333):
[7] Linear approximation for supersonic flow past a delta wing
Chen, Shuxing
Archive for Rational Mechanics and Analysis, 140 (04):
[8] PROBLEM OF MINIMAL DRAG OF CONICAL SUPERSONIC WING SURFACES WITH SUBSONIC LEADING EDGES
WAGNER, B
INGENIEUR ARCHIV, 1976, 45 (03): : 179 - 191
[9] ON THE CONCEPTUAL DESIGN OF SUPERSONIC CRUISING AIRCRAFT WITH SUBSONIC WING LEADING EDGES.
Torenbeek, E.
Delft progress report, 1983, 8 (01): : 55 - 80
[10] CROSS-FLOW SHOCK ON THE SUCTION SIDE OF A FLAT DELTA WING WITH SUPERSONIC LEADING EDGES
KUBO, S
FUJIMOTO, T
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1982, 24 (66) : 211 - 221

← 1 2 3 4 5 →