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
1988-01-01
Conference paper
No indication
English
AIAA | 1970
|Novel inlet–airframe integration methodology for hypersonic waverider vehicles
Online Contents | 2015
|