Supersonic external compression inlets are introduced, and the computational fluid dynamics (CFD) codes and tests needed to study flow associated with these inlets are outlined. Normal shock wave turbulent boundary layer interaction is discussed. Boundary layer control is considered. Glancing sidewall shock interaction is treated. The CFD validation of hypersonic inlet configurations is explained. Scramjet inlet modules are shown.
CFD (Computational Fluid Dynamics) Application to Supersonic/Hypersonic Inlet Airframe Integration
1988
62 pages
Report
Keine Angabe
Englisch
Aerodynamics , Jet & Gas Turbine Engines , Fluid Mechanics , Computational fluid dynamics , Engine airframe integration , Engine inlets , Hypersonic inlets , Inlet airframe configurations , Supersonic inlets , Boundary layer control , Flow visualization , Shock wave interaction , Supersonic combustion ramjet engines
Novel inlet–airframe integration methodology for hypersonic waverider vehicles
Online Contents | 2015
|AIAA | 1970
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