MODIFIED THIN SHOCK LAYER METHOD FOR SUPERSONIC-FLOW PAST AN OSCILLATING CONE

被引：5

作者：

HUI, WH ^{[1
]}

MAHOOD, GE ^{[1
]}

机构：

[1] UNIV WATERLOO,DEPT APPL MATH,WATERLOO,ONTARIO,CANADA

来源：

关键词：

D O I：

10.2514/3.27920

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：481 / 487

页数：7

共 25 条

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[2]

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COLE, JD .

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

[4] APPROXIMATION FOR HYPERSONIC FLOW PAST AN INCLINED CONE [J].

DOTY, RT ;

RASMUSSEN, ML .

[5]

FERRI A, 1950, TN2236 NACA

[6]

GUIRAUD JP, 1963, SUDAER154 STANF U, P176

[7]

HAYES WD, 1960, HYPERSONIC FLOW THEO, V1, pCH3

[8]

HUI WH, 1973, ASTRONAUT ACTA, V18, P35

[9]

HUI WH, 1975, AERONAUTICAL QUART, V24, P11

[10]

KOPAL Z, 1947, TR3 MASS I TECHN DEP