Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel

被引：0
|
作者：
K. Itoh
S. Ueda
H. Tanno
T. Komuro
K. Sato
机构：
[1] National Aerospace Laboratory,
[2] Kakuda,undefined
[3] Miyagi 981-1525,undefined
[4] Japan ,undefined
来源：
Shock Waves | 2002年 / 12卷
关键词：
Key words: Hypersonic flow, Aerothermodynamics, Scramjets;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A high enthalpy shock tunnel is a potential facility for gaining knowledge to develop modern aerothermodynamic and propulsion technologies. The largest high enthalpy shock tunnel HIEST was built at NAL Kakuda in 1997, aiming for aerothermodynamic tests of Japan's space vehicle HOPE and scramjet propulsion systems. Selected topics from the experimental studies carried out using HIEST so far, such as the nonequilibrium aerodynamics of HOPE, the surface catalytic effect on aerodynamic heating and scramjet performance are described.
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页码：93 / 98
页数：5
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