SHOCK-WAVE SHAPES ON HYPERSONIC AXISYMMETRIC POWER-LAW BODIES

被引：3

作者：

BEAVERS, GS

机构：

[1] University of Minnesota, Department of Aeronautics and Engineering Mechanics, Minneapolis, MN

来源：

关键词：

D O I：

10.2514/3.5510

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：2038 / &

共 9 条

[1]

CHENG HK, 1956, J AERONAUT SCI, V23, P700

[2] AN EXPERIMENTAL INVESTIGATION OF ASYMPTOTIC HYPERSONIC FLOWS [J].

FREEMAN, NC ;

CASH, RF ;

BEDDER, D .

[3]

FREEMAN NC, 1965, RESEARCH FRONTIERS F, P284

[4] INVISCID HYPERSONIC FLOW OVER PLANE POWER-LAW BODIES [J].

HORNUNG, HG .

[5]

HORNUNG HG, 1967, ARLA288 AUSTR DEF SC

[6]

KUBOTA T, 1957, 417 CAL I TECHN GRAD

[7] INVISCID HYPERSONIC FLOW OVER BLUNT-NOSED SLENDER BODIES [J].

LEES, L ;

KUBOTA, T .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (03) :195-202

[8]

Lees L., 1955, 5 INT AER C LOS ANG, P241

[9]

PECKHAM DH, 1965, MEASUREMENTS PRESSUR