USE OF THE HOT-WIRE ANEMOMETER AS A TRIGGERING AND TIMING DEVICE FOR WAVE PHENOMENA IN A SHOCK TUBE

被引：3

作者：

DOSANJH, DS

机构：

来源：

关键词：

D O I：

10.1063/1.1771243

中图分类号：

TH7 [仪器、仪表];

学科分类号：

0804 ; 080401 ; 081102 ;

摘要：

引用

页码：65 / 70

页数：6

共 13 条

[1]

BLEAKNEY, 1949, REV SCI INSTRUM, V20, P807

[2]

CORRSIN S, 1949, NACA1864 TECH NOT

[3]

DOSANJH, 1952, CM725 J HOPK U DEP A

[4]

DOSANJH DS, 1953, THESIS J HOPKINS U

[5]

GLASS, 1953, UTIA2 U TOR I AER RE

[6] ON THE SPEED OF SOUND IN GASES [J].

GLASS, II .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (04) :286-287

[7]

GLASS II, 1951, UTIA9 U TOR I AER RE

[8] STUDIES WITH AN AERODYNAMICALLY INSTRUMENTED SHOCK TUBE [J].

HERTZBERG, A ;

KANTROWITZ, A .

[9]

HUBER, 1949, NACA1903 TECH NOT

[10] TURBULENCE IN SUPERSONIC FLOW [J].

KOVASZNAY, LSG .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (10) :657-&