EFFECTS OF ATMOSPHERE AND AIRCRAFT MOTION ON THE LOCATION AND INTENSITY OF A SONIC BOOM

被引：34

作者：

FRIEDMAN, MP

KANE, EJ

SIGALLA, A

机构：

来源：

关键词：

D O I：

10.2514/3.1788

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1327 / 1335

页数：9

共 12 条

[1]

COURANT R, 1948, SUPERSONIC FLOW SHOC, P159

[2] GEOMETRICAL ACOUSTICS .1. THE THEORY OF WEAK SHOCK WAVES [J].

KELLER, JB .

[3]

RANDALL DG, 1957, RM3113 AER RES COUNC

[4]

RAO PS, 1956, AERONAUT QUART, V7, P21

[5]

RAO PS, 1956, AERONAUT QUART, V7, P135

[6]

REED JW, 1962, AEROSPACE ENG, V21, P66

WALKDEN, F .

AERONAUTICAL QUARTERLY, 1958, 9 (02) :164-194

[8]

WARREN CHE, 1954, TN2334 ROY AIRCR EST

[9] THE FLOW PATTERN OF A SUPERSONIC PROJECTILE [J].

WHITHAM, GB .

[10] ON THE PROPAGATION OF WEAK SHOCK WAVES [J].

WHITHAM, GB .