COMPRESSIBILITY EFFECTS IN UNSTEADY THIN-AIRFOIL THEORY

被引：35

作者：

AMIET, RK ^{[1
]}

机构：

[1] UNITED AIRCRAFT RES LABS,E HARTFORD,CT 06108

来源：

关键词：

D O I：

10.2514/3.49212

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：252 / 255

页数：4

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[2]

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[4]

Garrick I.E., 1957, AERODYNAMIC COMPONEN

GRAHAM, JMR .

[6]

Landahl M.T., 1961, UNSTEADY TRANSONIC F

[7] ON THE COMPRESSIBILITY CORRECTION FOR SUBSONIC UNSTEADY FLOW [J].

MILES, JW .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (03) :181-182

MILES, JW .

[9]

Miles JW, 1950, QUART APPLIED MATHEM, V8, P350

[10] UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW [J].

OSBORNE, C .