Mach 10 experimental database of a three-dimensional scramjet inlet flow field
An edition of Mach 10 experimental database of a three-dimensional scramjet inlet flow field (1995)
By Scott D. Holland
Publish Date
1995
Publisher
National Aeronautics and Space Administration, Langley Research Center,Available from the National Technical Information Service
Language
eng
Pages
214
Description:
subjects: Aerodynamics, Hypersonic, Air intakes, Airplanes, Computational fluid dynamics, Engine inlets, Flow distribution, Hypersonic Aerodynamics, Hypersonic speed, Inlet flow, Internal flow, Laminar boundary layer, Oblique shock waves, Pressure measurement, Ramjet engines, Scramjet engines, Shock wave interaction, Supersonic combustion ramjet engines, Three dimensional flow, Wind tunnel tests