探索发展激波风洞爆轰驱动技术
DEVELOPMENT STUDY OF DETONATION DRIVING TECHNIQUES FOR A SHOCK TUNNEL
查看参考文献20篇
|
文摘
|
发现了燃烧驱动激波管中入射激波马赫数异常升高的起因.实验显示爆轰驱动能力强于燃烧驱动，从而推动爆轰驱动技术的发展.采用卸爆管消除爆轰波反射高压以及双爆轰驱动段全部消除爆轰波后的Taylor稀疏波，使反向和前向爆轰驱动模式具有实用价值.反向爆轰驱动技术还成功用来延长激波风洞试验时间。 |
|
其他语种文摘
|
The cause for abnormal increase of shock Mach number in a combustion driven shock tube had been discovered. The experimental results show that the capabilities of gaseous detonation driver are stronger than to combustion driver which bring about a great advance in detonation driving technique. Using a dumping section to eliminate the reflected high pressure of the detonation wave and utilizing double detonation driver to eliminate completely the Taylor wave following the detonation wave makes the backward and forward detonation drivers usefulness. The backward detonation technique is utilized still to prolong the test duration for a shock tunnel. |
|
来源
|
力学学报
,2011,43(6):978-983 【核心库】
|
|
关键词
|
激波管
;
激波风洞
;
气体爆轰
|
|
地址
|
中国科学院力学研究所, 高温气体动力学国家重点实验室, 北京, 100190
|
|
语种
|
中文 |
|
文献类型
|
研究性论文 |
|
ISSN
|
0459-1879 |
|
学科
|
力学 |
|
基金
|
国家自然科学基金资助项目
|
|
文献收藏号
|
CSCD:4403205
|
参考文献 共
20
共1页
|
|
1.
Warren W R. A critique of high performance shock tube driving techniques.
Proc. 7th. Intern. Symp. on Shock Tubes,1969:143-176
|
CSCD被引
1
次
|
|
|
|
|
2.
Hertzberg A. A method for generation strong shock wave.
J Appl Phys,1954,25:130
|
CSCD被引
4
次
|
|
|
|
|
3.
俞鸿儒.
直通型激波风洞及其在传热实验中的应用.[学位论文],1963
|
CSCD被引
1
次
|
|
|
|
|
4.
钱学森. 致王寿云等六同志信.
钱学森现代军事科 学思想,2011:176-177
|
CSCD被引
1
次
|
|
|
|
|
5.
Bird G A.
A note on combustion driven shock tubes. RAE TN-Aero2511,1957
|
CSCD被引
2
次
|
|
|
|
|
6.
Waldron H F.
An experimental investigation of the flow properties behind strong shock waves in nitrogen. UTIA Rep. No 50,1958
|
CSCD被引
2
次
|
|
|
|
|
7.
Coates P B. A simple shock tubes with detonation driver gas.
Proc, Roy, Soc, (London), A,1965,283:18-32
|
CSCD被引
6
次
|
|
|
|
|
8.
Edwards D H. Pressure and velocity measurements on detonation waves in hydro-oxygen mixtures.
J Fluid Mechanics,1959,6:497-517
|
CSCD被引
3
次
|
|
|
|
|
9.
Yu H R. Recent developments in shock tube application.
Proc. 1989 Japanese Symp. on shock wave phenomena,1989:1-9
|
CSCD被引
1
次
|
|
|
|
|
10.
Yu H R. Gaseous detonation driver for a shock tunnel.
Shock Waves,1992,2(4):245-254
|
CSCD被引
21
次
|
|
|
|
|
11.
Bakos R J.
Option for enhancement of the performance of shock-expansion tubes and tunnels. AIAA 95-0799,1995
|
CSCD被引
1
次
|
|
|
|
|
12.
Yu H R. Oxy-hydrogen combustion and detonation driven shock tube.
Acta Mechanica Sinica,1999,15(2):97-107
|
CSCD被引
9
次
|
|
|
|
|
13.
Fuehrer R G. Measurements of incident shock test time and reflected shock pressure at full turbulent boundary layer test condition.
Shock tubes,1970:31-59
|
CSCD被引
1
次
|
|
|
|
|
14.
Jiang Z L. Forward-running detonation drivers for high-enthalpy shock tunnels.
AIAA Journal,2002,40(10):2009-2016
|
CSCD被引
17
次
|
|
|
|
|
15.
Bakos R J.
An experimental and computational study leading to new test capabilities for the hypulse facility with a detonation driver. AIAA 96-2193,1996
|
CSCD被引
1
次
|
|
|
|
|
16.
陈宏. 用于激波管/风洞的双爆轰驱动段.
中国科学 G 辑,2004,34(2):183-191
|
CSCD被引
7
次
|
|
|
|
|
17.
Lu F K. Advenced Hypersonic Test Facilities.
Progress in Astronautics and Aeronautics Volume 198,2002
|
CSCD被引
3
次
|
|
|
|
|
18.
Holden M.
Large Energy National Shock Tunnel(LENS), description and capabilities brochure, Calspan-UB research Center,1991
|
CSCD被引
1
次
|
|
|
|
|
19.
. 8个重大科研装备自主创新项目启动.
人民日报(第2版),2008
|
CSCD被引
18
次
|
|
|
|
|
20.
涂元季.
人民科学家钱学森,2002
|
CSCD被引
6
次
|
|
|
|
|
了解气象卫星更多信息，请访问