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

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[3]

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[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 [J].

CHENG, HK .

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[9]

CHENG HK, 1954, J RATIONAL MECHANICS

[10]

CHENG HK, BELL AIRCRAFT CORPOR, V1