Unsteady, Finite-Rate Model for Application in the Design of Complete Gas-Turbine Combustor Configurations
Symposium, Design principles and methods for aircraft gas turbine engines ; 1998 ; Toulouse; France
1999-01-01
17 pages
Conference paper
English
RTO , aircraft engines , AVT
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
TIBKAT | 2012
|