Euler and Navier-Stokes Analysis of Supersonic Flow Around an 8-Fin or Ring-Wing-3-Fin Stabilized Missile
European forum, Recent developments and applications in aeronautical CFD ; 1993 ; London
01.01.1993
21.1-21.14
1; v.; various pagings
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Euler and Navier-Stokes Solutions for Supersonic Flow Around a Complex Missile
Online Contents | 1994
|Navier-Stokes Simulation Methodology for Supersonic Missile Inlets
British Library Conference Proceedings | 1997
|