UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW

被引：28

作者：

OSBORNE, C ^{[1
]}

机构：

[1] CORNELL UNIV,ITHACA,NY 14850

来源：

关键词：

D O I：

10.2514/3.6730

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：205 / 209

页数：5

共 13 条

[1] AERODYNAMIC NOISE OF SMALL-PERTURBATION SUBSONIC FLOWS [J].

AMIET, R ;

SEARS, WR .

[2]

Drischler J.A, 1956, 3748 NASA TN

[3]

FUNG YC, 1955, THEORY AEROELASTICIT, P418

[4]

GARRICK IE, 1957, NON STEADY WING CH F, V7

GRAHAM, JMR .

[6]

JOHNSON W, 1970, TR1532 AER STRUCT RE

KEMP, NH .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (10) :713-714

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

MILES, JW .

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

[9]

OSBORNE C, 1971, THESIS CORNELL U

[10]

Sears R.W., 1938, THESIS CALIFORNIA I