Pressure Gradient Effects on Hypersonic Cavity Flow Heating

The effect of a pressure gradient on the local heating disturbance of rectangular cavities tested at hypersonic freestream conditions has been globally assessed using the two-color phosphor thermography method. These experiments were conducted in the Langley 31-Inch Mach 10 Tunnel and were initiated...

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Bibliographische Detailangaben

Hauptverfasser:	Everhart, Joel L., Alter, Stephen J., Merski, N. Ronald, Wood, William A., Prabhu, Ramadas K.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics
Online-Zugang:	Volltext bestellen
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