Study of Total Pressure Losses at the Engine Face of a Submerged Inlet with an Ingested Vortex
German aerospace aerodynamics and the german society for aeronautics and astronautics (Symposium)
German aerospace aerodynamics and the german society for aeronautics and astronautics (Symposium) ; 361-374
01.01.2018
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
INGESTED PARTICLE REDISTRIBUTION IN A SERPENTINE ENGINE INLET
TIBKAT | 2020
|Computational Study of a High-Performance Submerged Inlet with Bleeding Vortex
Online Contents | 2012
|