中国开放科研知识云: 检索

Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8
作者: Wang WT(王文韬); Wang Q(汪球); Li JP(李进平); Zhao W(赵伟); Gao, Liangjie

收藏 | 浏览/下载：0/0 | 提交时间：2024/02/26

Finite Element Method Hypersonic Shock Tube/Tunnel Diaphragm Burst Pressure

Characterization of reflected shock tunnel air conditions using a simple method 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 5, 页码: 17
作者: Gu, Sangdi; Olivier, Herbert; Wen, Chih-Yung; Hao, Jiaao; Wang, Qiu

收藏 | 浏览/下载：32/0 | 提交时间：2022/07/18

China's Detonation-driven Shock Tube Wind Tunnels: A Case Study of Transnational Science in Aeronautics during the Cold War 期刊论文
EAST ASIAN SCIENCE TECHNOLOGY AND SOCIETY-AN INTERNATIONAL JOURNAL, 2021, 页码: 28
作者: Zhihu, Zhang; Seely, Bruce E.

收藏 | 浏览/下载：9/0 | 提交时间：2022/07/01

Shock tubes wind tunnels China international collaboration technology transfer research & development aerospace technology Cold War

The Richtmyer-Meshkov instability of concave circular arc density interfaces in hydrodynamics and magnetohydrodynamics 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 3, 页码: 16
作者: Qin JH(秦建华); Dong GD(董国丹)

收藏 | 浏览/下载：38/0 | 提交时间：2021/05/06

A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
作者: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)

收藏 | 浏览/下载：21/0 | 提交时间：2020/11/30

calorimeter shock tunnel heat transfer measurement hypersonic

Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)

收藏 | 浏览/下载：16/0 | 提交时间：2020/11/30

Quasi-one-dimensional Detonation Shock tunnel Shock speed

Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
作者: Wang Q(汪球); Luo K(罗凯); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)

收藏 | 浏览/下载：37/0 | 提交时间：2020/08/26

Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow

Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
作者: Wang YP(汪运鹏); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)

收藏 | 浏览/下载：12/0 | 提交时间：2017/09/19

爆轰驱动膨胀管性能研究 期刊论文
航空学报, 2016, 卷号: 37, 期号: 3, 页码: 810-816
作者: 周凯; 汪球; 胡宗民; 姜宗林

收藏 | 浏览/下载：29/0 | 提交时间：2016/12/16

hypervelocity detonation-driven expansion tube performance study experimental tests numerical simulation

Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Flow 期刊论文
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 页码: 435,440
Masashi KASHITANIl; Keita MIURAl; Shinichiro NAKA02; Yutaka YAMAGUCHI2

收藏 | 浏览/下载：17/0 | 提交时间：2013/01/31

Shock tube Aerodynamics Transonic flows Aspect ratio Wind tunnel correction

在结果中检索

相关链接

CORC

联系我们