Drag and Total Power Reduction for Artificial Heat Input in Front of Hypersonic Blunt Bodies

The effect of an air-spike in hypersonic flow is considered in the paper. The similarity laws of shape dependence and shock wave parameters, as a function of the strength of the heat source and characteristics of incident flow, are given. The numerical modeling is performed, based on the Euler gasdy...

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Bibliographische Detailangaben

Hauptverfasser:	Myrabo, L N, Raize, Yu P, Shneider, M N
Format:	Tagungsbericht
Sprache:	eng
Online-Zugang:	Volltext
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