NASA NTRS · 19890007382
CFD application to subsonic inlet airframe integration
Abstract
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.
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Anderson, Bernhard H.. 1988-01-01. CFD application to subsonic inlet airframe integration. https://ntrs.nasa.gov/citations/19890007382
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