3D Turbulent Flow at Compressor Rotor Exit under Different Flow Conditions
JOURNAL OF AEROSPACE POWER ; 12 , 3 ; 268-272
1997-01-01
5 pages
Aufsatz (Zeitschrift)
Englisch
DDC: | 629.1 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Mixed Flow Turbines: Inlet and Exit Flow Under Steady and Pulsating Conditions
Online Contents | 2001
|DOAJ | 2020
|