中国开放科研知识云: 检索

A Multi-space Interrelation Theory for Correlating Aerodynamic Data from Hypersonic Ground Testing 会议论文
Nagoya, Japan, 2017-07-9~14
作者: Jiang ZL(姜宗林); Luo ZT(罗长童)

收藏 | 浏览/下载：34/0 | 提交时间：2020/01/06

Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文
Nagoya, Japan, 2017-07-9~14
作者: Liu YF(刘云峰); Wang YP(汪运鹏); Yuan CK(苑朝凯); Luo ZT(罗长童); Jiang ZL(姜宗林)

收藏 | 浏览/下载：39/0 | 提交时间：2020/01/06

AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
Montreal, CANADA, JUL 15-20, 2018
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林); Teng HH(滕宏辉)

收藏 | 浏览/下载：29/0 | 提交时间：2019/04/19

Assessment of Grids and Computational Schemes for Numerical Simulation of HIFiRE-5 会议论文
Proceedings of 2018 9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018
作者: Han, Z.; Yan, C.; Liu, H.

收藏 | 浏览/下载：13/0 | 提交时间：2019/12/30

Aerospace engineering Boundary layer flow Boundary layers Discrete event simulation Hypersonic flow Numerical methods Numerical models Wind tunnels Calculation results Complex flow structures Computational schemes Grid resolution HIFiRE-5 Reconstruction method Spatial discretization methods Wind tunnel test models Computational fluid dynamics

The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
Xiamen, China, 6-9 March 2017
作者: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)

收藏 | 浏览/下载：19/0 | 提交时间：2018/01/16

Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels

Experimental Study of a Scramjet Engine Intake with a Hypersonic Wind Tunnel 会议论文
ISABE, Busan,KOREA, 2013
Sang Hun Kang; Yang Ji Lee; Soo Seok Yang

收藏 | 浏览/下载：7/0 | 提交时间：2013/11/29

Concept of non-ablative thermal protection system for hypersonic vehicles 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
作者: Jiang ZL(姜宗林); Liu YF(刘云峰)

收藏 | 浏览/下载：23/0 | 提交时间：2013/12/12

A New Evolutionary Algorithm for Ground to Flight Data Correlation 会议论文
7th East Asia SIAM Conference, Kitakyushu Campus, Waseda University, Japan, June 27-29, 2011
作者: Luo CT(罗长童); Zhang SL(张绍良); Jiang ZL(姜宗林)

收藏 | 浏览/下载：18/0 | 提交时间：2013/03/05

Conceptual Study on Non-ablative TPS for Hypersonic Vehicles 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
作者: Jiang ZL(姜宗林); Liu YF(刘云峰); Han GL(韩桂来); Jiang ZL(姜宗林)

收藏 | 浏览/下载：41/0 | 提交时间：2014/02/24

Experimental investigation of cavity-based scramjet model 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者: Gu HB(顾洪斌); Chen LH(陈立红); 张新宇(Chang XY)

收藏 | 浏览/下载：11/0 | 提交时间：2017/06/01

Kerosene fuel Mass flow rate Scramjet engine

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