OSCILLATING AIRFOILS .2. NEWTONIAN FLOW THEORY AND APPLICATION TO POWER-LAW BODIES IN HYPERSONIC FLOW

被引：4

作者：

BARRON, RM ^{[1
]}

MANDL, P ^{[1
]}

机构：

[1] CARLETON UNIV,DEPT MATH,OTTAWA K1S 5B6,ONTARIO,CANADA

来源：

关键词：

D O I：

10.2514/3.61019

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1132 / 1138

页数：7

共 10 条

[1]

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[2] NEWTONIAN FLOW PAST POWER-LAW BODIES [J].

BARRON, RM .

[3]

BARRON RM, 1974, THESIS CARLETON U

[4] NEWTONIAN FLOW THEORY FOR SLENDER BODIES [J].

COLE, JD .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (06) :448-455

[5]

Garabedian P.R., 1964, PARTIAL DIFFERENTIAL

[6]

GUIRAUD JP, 1965, BASIC DEV FLUID DYNA, V1

[7]

MCINTOSH SC, 1965, THESIS STANFORD U

[8]

NOBLE B, 1969, APPLIED LINEAR ALGEB, P361

[9]

VANDYKE MD, 1954, NACA1183 REP

[10]

Whittaker ET., 1935, MODERN ANAL