NOTE ON THE USE OF THE SHOCK TUBE AS AN INTERMITTENT SUPERSONIC WIND TUNNEL

被引：2

作者：

RUDINGER, G

机构：

来源：

PHYSICAL REVIEW | 1949年 / 75卷 / 12期

关键词：

D O I：

10.1103/PhysRev.75.1948

中图分类号：

O4 [物理学];

学科分类号：

0702 ;

摘要：

引用

页码：1948 / 1949

页数：2

共 50 条

[1] STARTING PHENOMENA IN A SUPERSONIC TUBE WIND TUNNEL
JOHNSON, JA
CAGLIOST.D
AIAA JOURNAL, 1971, 9 (01) : 101 - &
[2] A SUPERSONIC, INTERMITTENT, MOVABLE WIND TUNNEL FOR OPTICAL STUDIES
LADENBURG, R
VANVOORHIS, CC
WINCKLER, J
PHYSICAL REVIEW, 1948, 74 (09): : 1229 - 1229
[3] THE LUDWIEG PRESSURE-TUBE SUPERSONIC WIND TUNNEL
CABLE, AJ
COX, RN
AERONAUTICAL QUARTERLY, 1963, 14 (02): : 143 - 157
[4] SOME EXPERIMENTS WITH A RESONANCE TUBE IN A SUPERSONIC WIND TUNNEL
SIBULKIN, M
VREBALOVICH, T
JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (07): : 465 - 466
[5] A NOTE ON THE DESIGN OF SUPERSONIC WIND-TUNNEL NOZZLES
MEYER, RE
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (02): : 140 - 141
[6] Determination of starting shock velocity in supersonic wind tunnel
Disimile, P.J., 1981, American Inst. Aeronautics and Astronautics Inc., United States (33):
[7] SHOCK OBSERVATIONS IN A CONTINUOUS SUPERSONIC PLASMA WIND TUNNEL
BARTOLI, C
BITTER, M
NUOVO CIMENTO DELLA SOCIETA ITALIANA DI FISICA B, 1971, B 5 (01): : 95 - &
[8] Investigation of the operation of an intermittent supersonic blowdown and suction wind tunnel
Bezmenov, V.Ya.
Fluid mechanics. Soviet research, 1988, 17 (06): : 87 - 98
[9] DETERMINATION OF STARTING SHOCK VELOCITY IN SUPERSONIC WIND-TUNNEL
DISIMILE, PJ
TOY, N
AIAA JOURNAL, 1995, 33 (10) : 1981 - 1983
[10] Numerical simulations of the shock train in the diffuser of a supersonic wind tunnel
Chen, Jiming
Ren, Yuxin
Qinghua Daxue Xuebao/Journal of Tsinghua University, 2007, 47 (02): : 264 - 267

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