AERODYNAMICS OF A RECTANGULAR PLATE WITH VORTEX SEPARATION IN SUPERSONIC FLOW

被引：5

作者：

CHENG, HK

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1955年 / 22卷 / 04期

关键词：

D O I：

10.2514/8.3314

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：217 / 226

页数：10

共 35 条

[1] LEADING-EDGE SEPARATION FROM DELTA-WINGS AT SUPERSONIC SPEEDS
ADAMS, MC
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (06): : 430 - 430
[2] SLENDER-BODY THEORY - REVIEW AND EXTENSION
ADAMS, MC
SEARS, WR
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (02): : 85 - 98
[3] BETZ A, 1935, AERODYNAMIC THEORY, V6, pCH2
[4] BOLLAY W, 1936, J AERONAUTICAL SCIEN, V4, P294
[5] BROWN CE, 1946, NACA TN1183
[6] BROWN CE, 1954, 22ND ANN M IAS PAP
[7] BUSEMANN A, 1942, INFINITESIMALE KEGEL, P455
[8] REMARKS ON NONLINEAR LIFT AND VORTEX SEPARATION
CHENG, HK
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (03): : 212 - 214
[9] CHENG HK, 1954, J RATIONAL MECHANICS
[10] CHENG HK, BELL AIRCRAFT CORPOR, V1