Parametric study of injector radial penetration on stalling characteristics of a transonic fan-Reference-Cited by-同舟云学术

Parametric study of injector radial penetration on stalling characteristics of a transonic fan

Published:2017-07 Issue: Volume:66 Page:112-118
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Khaleghi Hossein^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

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4. Effects of endwall suction and blowing on compressor stability enhancement;Lee;ASME J. Turbomach.,1990

5. Active suppression of rotating stall and surge in axial compressors;Day;ASME J. Turbomach.,1993

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