Numerical Simulation of the Effect of Inlet Distortion to the Subsonic Axial-Flow Compressor
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
2008-01-01
8 pages
Conference paper
English
Aerospace , AIAA , Aeronautics , Astronautics
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Statistical averages of subsonic inlet distortion
AIAA | 1974
|Numerical Investigation of Tandem Airfoils for Subsonic Axial-Flow Compressor Blades
Online Contents | 2009
|British Library Online Contents | 2008
|