Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
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Article title
Parametric study of injection angle effects on stability of transonic axial compressors
Type
D - Journal article
DOI
Title of journal
Journal of Propulsion and Power
Article number
-
Volume number
24
Issue number
5
First page of article
1100
ISSN of journal
0748-4658
Year of publication
2008
URL
-
Number of additional authors
3
Additional information
This research provided insight into mechanisms of transonic axial compressor stability enhancement through case injection and examined the potential for performance improvement at off-design operation regimes. This research has led to the demonstration of cost-effective methodologies that help to reduce the performance degradation under near-stall conditions in transonic compressors. The case injection concept has attracted interest in the high speed turbomachinery sector being adopted in research papers of leading aerospace companies, GE Global Research and GE Aviation, United States.
Interdisciplinary
-
Cross-referral requested
-
Research group
B - Computational Science & Engineering
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-