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  5. Mach reflection in steady flowⅠ.Mikhail Ivanovs contributions Ⅱ.Caltech stability experiments

Mach reflection in steady flowⅠ.Mikhail Ivanovs contributions Ⅱ.Caltech stability experiments

来源 :29th International Symposium on Rarefied Gas Dynamics(第29届国际 | 被引量 : 0次 | 上传用户：e3e45r
【摘 要】
：
In steady supersonic flow at sufficiently high Mach number,there exists a range of incident shock angles within which both regular and Mach reflection are possi
【作 者】
：
Hans G.Hornung 
【机 构】
：
GraduateAerospaceLaboratories,CaliforniaInstituteofTechnology,Pasadena91125,USA
【出 处】
：
29th International Symposium on Rarefied Gas Dynamics(第29届国际
【发表日期】
：
2014年7期
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In steady supersonic flow at sufficiently high Mach number,there exists a range of incident shock angles within which both regular and Mach reflection are possible.
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