Corner Effects in Oblique Shock Wave/ Boundary Layer Interactions in Rectangular Channels (AIAA 2017-0984)
55th AIAA Aerospace Sciences Meeting 2017 ; 2017 ; Grapevine, Texas
01.01.2017
11 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.