AIAA-2005-1221 FIRST STAGE OF THE CENTRIFUGAL COMPRESSOR DESIGN WITH TANDEM ROTOR BLADES
17th, International symposium on air breathing engines ; 2005 ; Munich, Germany
2005-01-01
187 pages
Includes bibliographical references and index; Papers on CD-ROM
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA-2005-1222 TWO-STAGE SINGLE-SHAFT CENTRIFUGAL COMPRESSOR ADVANCED DESIGN
British Library Conference Proceedings | 2005
|AIAA-2005-1058 BOUNDARY LAYER DEVELOPMENT ON ROTOR BLADES OF A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR
British Library Conference Proceedings | 2005
|British Library Conference Proceedings | 2005
|AIAA-2005-1182 A 3D HYBRID DESIGN METHOD OF COMPRESSOR BLADES
British Library Conference Proceedings | 2005
|