Total Unsteadiness Analysis for an Axial-Flow Compressor Rotor
36th, Aerospace sciences meeting ; 1998 ; Reno; NV
1998-01-01
ALL
Nos AIAA 98-0001 to 98-1069 with gaps held only
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
An experimental study of rotor-stator wake unsteadiness in a multistage axial compressor
SAGE Publications | 2021
|Flow Field Unsteadiness in the Tip Region of a Transonic Compressor Rotor
British Library Online Contents | 1994
|