Pressure-fluctuation inputs and response of panels underlying attached and separated supersonic turbulent boundary layers

Results are presented for an investigation of surface pressure fluctuations and response of panels underlying attached and separated turbulent boundary layers and shock waves. Tests conducted at transonic and supersonic Mach numbers to 3.6 to study the pressure fields. Assorted fixed edge flat panel...

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Bibliographische Detailangaben

Hauptverfasser:	Coe, C. F., Chyu, W. J.
Format:	Report
Sprache:	eng
Schlagworte:	Fluid Mechanics
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