Aeroheating predictions for X-34 using an inviscid-boundary layer method

An edition of Aeroheating predictions for X-34 using an inviscid-boundary layer method (1998)

Aeroheating predictions for X-34 using an inviscid-boundary layer method

By Christopher J. Riley

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Publish Date

1998

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Convective heat transfer, X-34 reusable launch vehicle, Boundary layers, Algorithms, Aerodynamic heating, Inviscid flow, Turbulent flow, Surface temperature, Mathematical models, Hypersonics