AIAA 2006-0419 Axial Compressor Rotor Flow Structure at Stall-Inception
44th, AIAA aerospace sciences meeting ; 2006 ; Reno, NV
2006-01-01
11 pages
See also RMS for papers held on microfiche
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Axial Compressor Rotor Flow Structure at Stall-Inception
AIAA | 2006
|Numerical and experimental research of stall inception on subsonic axial-flow compressor rotor
SAGE Publications | 2010
|Numerical and experimental research of stall inception on subsonic axial-flow compressor rotor
Online Contents | 2010
|An Explanation for Flow Features of Spike-Type Stall Inception in an Axial Compressor Rotor
Online Contents | 2013
|An Explanation for Flow Features of Spike-Type Stall Inception in an Axial Compressor Rotor
Online Contents | 2013
|