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Development and calibration of detonation-driven high-enthalpy and hypersonic test facilities
Jiang ZL(姜宗林); Yu HR(俞鸿儒)
2016
Other Abstract

Hypersonics for the foreseeable future is the domain of space access and hypersonic flight. A hypersonic vehicle encounters an aero-thermodynamic environment characterized by strong shocks and high temperatures, and the flow in the hypersonic regime behaves quite differently from that at supersonic Mach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, 1994; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1989; Anderson in Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York, 1989).

Source PublicationExperimental Methods of Shock Wave Research
Pages285-313
PublisherSpringer
Publication PlaceNew York
Language英语
ISBN9783319237442
Document Type图书章节
Identifierhttp://dspace.imech.ac.cn/handle/311007/77971
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
Jiang ZL,Yu HR. Development and calibration of detonation-driven high-enthalpy and hypersonic test facilities[Ch]. Experimental Methods of Shock Wave Research,Springer,2016.
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