A Structured Mesh Euler and Interactive Boundary Layer Method for Wing/Body Configurations
CHINESE JOURNAL OF AERONAUTICS ; 21 , 1 ; 19-27
2008-01-01
9 pages
Article (Journal)
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Boundary-layer-induced secondary flows on wing-body configurations
Tema Archive | 1980
|The 3-D Euler Solution Around Wing-Body Configurations
AIAA | 2002
|