MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY

MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY

The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,0...

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Bibliographische Detailangaben
Hauptverfasser: Tabakoff,Widen, mcDonel,James D
Format: Report
Sprache:eng
Schlagworte:
DUCT INLETS
Fluid Mechanics
GEOMETRIC FORMS
HEAT TRANSFER
HYPERSONIC FLOW
LAMINAR BOUNDARY LAYER
MEASUREMENT
Thermodynamics
TWO DIMENSIONAL
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Beschreibung
Zusammenfassung:The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. (Author)