High-Speed Centrifugal Compressor Instabilities during Speed Transients-Reference-Cited by-同舟云学术

High-Speed Centrifugal Compressor Instabilities during Speed Transients

Published:2004-07 Issue:3 Volume:17 Page:106-112
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Oakes William C.¹,Lawless Patrick B.²,Fleeter Sanford³

Affiliation:

1. Assistant Professor, School of Mechanical Engineering, Perdue Univ., West Lafayette, IN 47907.

2. Associate Professor, School of Mechanical Engineering, Perdue Univ., West Lafayette, IN 47907.

3. McAllister Distinguished Professor, School of Mechanical Engineering, Perdue Univ., West Lafayette, IN 47907.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282004%2917%3A3%28106%29

Reference9 articles.

1. Stall Inception in Axial Flow Compressors

2. Day I. J. and Freeman C. (1993). “Unstable behavior of low- and high-speed compressors.” American Society of Mechanical Engineer Cincinnati Paper 93-GT-26.

3. Distinction Between Different Types of Impeller and Diffuser Rotating Stall in a Centrifugal Compressor With Vaneless Diffuser

4. Rotating waves as a stall inception indication in axial compressors.;Garnier V. H.;ASME J. Turbomach.,1990

5. Lawless P. B. and Fleeter S. (1993). “Rotating stall acoustic signature in a low-speed centrifugal compressor. II. Vaned diffuser.” American Society of Mechanical Engineer Cincinnati Paper 93-GT-254.

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