NUMERICAL COMPARISON BETWEEN EXACT AND APPROXIMATE THEORIES OF HYPERSONIC INVISCID FLOW PAST SLENDER BLUNT NOSED BODIES

被引：5

作者：

FELDMAN, S

机构：

来源：

ARS JOURNAL | 1960年 / 30卷 / 05期

关键词：

D O I：

10.2514/8.5120

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：463 / 468

页数：6

共 13 条

CASACCIO, A .

JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (01) :63-64

[2]

FERRI A, 1958, AD155822

[3]

FERRI A, 1956, WADC TN560294

[4]

Hayes W. D., 1959, HYPERSONIC FLOW THEO

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

LEES, L ;

KUBOTA, T .

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

[6] DYNAMICS OF A DISSOCIATING GAS .1. EQUILIBRIUM FLOW [J].

LIGHTHILL, MJ .

[7] CYLINDRICAL SHOCK WAVES PRODUCED BY INSTANTANEOUS ENERGY RELEASE [J].

LIN, SC .

[8]

OPIK EJ, 1958, PHYSICS METEOR FLIGH

[9] ON THE PROPAGATION AND STRUCTURE OF THE BLAST WAVE .1. [J].

SAKURAI, A .

[10] ON THE PROPAGATION AND STRUCTURE OF A BLAST WAVE, .2. [J].

SAKURAI, A .