Asymmetry Effects in Numerical Simulation of Supersonic Flows with Upstream Separated Regions
39th, Aerospace sciences meeting ; 2001 ; Reno, NV
01.01.2001
ALL
Paper nos AIAA-2001-0003 to AIAA-2001-0660 with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Numerical simulation of separated supersonic flows around tactical missile bodies
Tema Archiv | 1988
|Separated supersonic and subsonic flows
NTRS | 1955
|