EFFECTS OF COMPRESSIBILITY ON DYNAMIC STALL

被引：11

作者：

FUNG, KY

CARR, LW

机构：

[1] NASA,AMES RES CTR,USA,AEROFLIGHTDYNAM DIRECTORATE,MOFFETT FIELD,CA 94035

[2] NASA,AMES RES CTR,FLUID DYNAM RES BRANCH,MOFFETT FIELD,CA 94035

来源：

AIAA JOURNAL | 1991年 / 29卷 / 02期

基金：

美国国家航空航天局;

关键词：

D O I：

10.2514/3.10578

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：306 / 308

页数：3

共 13 条

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CARR, LW .

JOURNAL OF AIRCRAFT, 1988, 25 (01) :6-17

[2]

CARR LW, 1982, HOT WIRE HOT FILM ME, V3

[3]

DADONE LU, 1977, NASA CR2914

[4] SHOCK-INDUCED DYNAMIC STALL [J].

ERICSSON, LE ;

REDING, JP .

JOURNAL OF AIRCRAFT, 1984, 21 (05) :316-321

[5]

HARPER PW, 1950, NACA TN2061

[6]

KATARY M, 1983, AIAA832133 PAP

[7]

LORBER PF, 1987, AIAA871329 PAP

[8]

McCroskey W. J., 1981, J AM HELICOPTER SOC, V26, P40, DOI [10.4050/JAHS.26.40, DOI 10.4050/JAHS.26.40]

[9]

MCCROSKEY WJ, 1982, NASA TM84245

[10] ON THE NON-EXISTENCE OF CONTINUOUS TRANSONIC FLOWS PAST PROFILES .2. [J].

MORAWETZ, CS .

COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1957, 10 (01) :107-131

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