Recent development of casing treatments for aero-engine compressors-Reference-Cited by-同舟云学术

Recent development of casing treatments for aero-engine compressors

Published:2019-01 Issue:1 Volume:32 Page:1-36
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

SUN Xiaofeng,DONG Xu,SUN Dakun

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference59 articles.

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2. Koch CC. Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, Part VI—Final report. Washington, D.C.: NASA; 1970. Report No.: NASA CR-54592.

3. Stall margin improvement by casing treatment—Its mechanism and effectiveness;Takata;ASME J Eng Power,1977

4. Kang CS, McKenzie AB, Elder RL. Recessed casing treatment effects on fan performance and flow field. New York: ASME; 1995. Report No.: 95-GT-197

5. Fabri J, Reboux J. Effect of outer casing treatment and tip clearance on stall margin of a supersonic rotating cascade. New York: ASME; 1975. Report No.: 75-GT-95.

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