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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [2]
俞鸿儒 [1]
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Creator：姜宗林
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Document Type：会议论文
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Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
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View/Download：551/78
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Submit date：2020/01/06
The applicability of Mach number independence principle in case of hypersonic thermo-chemical nonequilibrium flow
会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012
Authors:
Li K(李康)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
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View/Download：645/149
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Submit date：2015/03/02
Keywords: Mach Number Independence
Oswatitsch
Nonequilibrium Flow
Real-gas Effect
Expansion Effect
