The symposium focused on departures from the classical boundary layer theories toward shock wave-boundary layer interactions with their attendant flow separation and reattachment and toward the three-dimensional viscous interactions of practical configurations. It thus dealt with one of the key problem areas associated with high speed supersonic aircraft, lifting-reentry vehicles, and potential hypersonic cruise vehicles. Such configurations are highly three-dimensional with complex flows involving strong viscous-inviscid interactions in regions of compression such as in air breathing engine inlets, at wing-body junctions, and over control surfaces. (Author)
Viscous Interaction Phenomena in Supersonic and Hypersonic Flow
1970
566 pages
Report
No indication
English
Viscous interaction phenomena in hypersonic wedge flow
AIAA | 1995
|Viscous Interaction Phenomena in Hypersonic Wedge Flow
Online Contents | 1995
|Dynamic Viscous Pressure Interaction in Hypersonic Flow
NTIS | 1970
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