A THEORETICAL AND EXPERIMENTAL STUDY OF FINITE AMPLITUDE WAVE INTERACTIONS WITH CHANNELS OF VARYING AREA

被引：11

作者：

KAHANE, A

WARREN, WR

GRIFFITH, WC

MARINO, AA

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 08期

关键词：

D O I：

10.2514/8.3112

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：505 / &

共 16 条

[1]

ASCHENBRENNER J, 1937, FORSCH INGENIEURWES, V8, P118

[2] THE SHOCK TUBE - A FACILITY FOR INVESTIGATIONS IN FLUID DYNAMICS [J].

BLEAKNEY, W ;

WEIMER, DK ;

FLETCHER, CH .

[3]

BULL V, 1951, 12 U TOR I AER REP

[4]

Courant R., 1948, SUPERSONIC FLOW SHOC

[5]

CROCCO L, 1932, NACA TN690

[6] THE MACH REFLECTION OF SHOCK WAVES AT NEARLY GLANCING INCIDENCE [J].

FLETCHER, CH ;

TAUB, AH ;

BLEAKNEY, W .

[7]

GUDERLEY G, 1948, NACA TM1196

[8]

HERZBERG A, 1950, J APP PHYS, V21, P874

[9]

HESS RV, 1949, NACA TN1878

[10]

HOWES WL, 1952, NACA TN2693