HEATING CHARACTERISTICS OF BLUNT SWEPT FIN-INDUCED SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION

An experimental study was conducted on shock wave turbulentboundary layer interactions caused by a blunt swept fin-plate configuration at Machnumbers of 5.0, 7.8, 9.9 for a Reynolds number range of (1.0.～4.7)×10~7/m. Detailedheat transfer and pressure distributions were measured at fin deflection an...

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Veröffentlicht in:	Acta mechanica Sinica 1998-05, Vol.14 (2), p.139-146
1. Verfasser:	唐贵明
Format:	Artikel
Sprache:	eng
Schlagworte:	boundary fin flow heat hypersonic interaction layer shock transfer wave
Online-Zugang:	Volltext
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