The fluid dynamics of curved diffuser duct flows of military aircraft is discussed. Three-dimensional parabolized Navier-Stokes analysis, and experiment techniques are reviewed. Flow measurements and pressure distributions are shown. Velocity vectors, and the effects of vortex generators are considered.
CFD application to subsonic inlet airframe integration
01.01.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA | 1970
|Novel inlet–airframe integration methodology for hypersonic waverider vehicles
Online Contents | 2015
|