The research was designed to gain understanding of the flow of air at high speeds over the components of lifting supersonic and hypersonic vehicles--wings, flaps, fins, inlets--and their interactions with respect to heating, surface friction, pressure, and aerodynamic forces. The objective was to help predict (a) flows on complex aerospace vehicle configurations in high-speed flight and (b) the location of areas of high heating. The research covers the areas of laminar and turbulent boundary layers, boundary layer transition, boundary layer separation, base flows and wakes, low density flows, three-dimensional interactions, viscous flow problems, and some flow measurement techniques.
Viscous Flow Interaction Studies
1975
53 pages
Report
No indication
English
Fluid Mechanics , Aerodynamics , Viscous flow , Supersonic characteristics , Hypersonic characteristics , Lifting bodies , Laminar boundary layer , Turbulent boundary layer , Boundary layer transition , Interactions , Base flow , Couette flow , Low density , Aerospace craft , Aerodynamic heating , Mathematical prediction , Wake , Measuring instruments
Viscous flow interaction studies
Tema Archive | 1975
|Viscous-inviscid interaction in transonic flow
AIAA | 1981
|Viscous Interaction Phenomena in Hypersonic Wedge Flow
Online Contents | 1995
|Dynamic Viscous Pressure Interaction in Hypersonic Flow
NTIS | 1970
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