Development of a coupled supersonic inlet-fan Navier–Stokes simulation method
Chinese journal of aeronautics ; 31 , 2 ; 237-246
01.01.2018
10 pages
Aufsatz (Zeitschrift)
Englisch
DDC: | 629.13005 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Supersonic inlet study using the Navier-Stokes equations
AIAA | 1986
|Prediction of Supersonic Inlet Performances with 3-D Navier-Stokes Calculations
British Library Conference Proceedings | 1997
|