Conference item

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Abstract:: Large tip clearances typically in the region of 6% exist in the high pressure (HP) stages of compressors of industrial gas turbines. Due to the relatively short annulus height and significant blockage, the tip clearance flow accounts for the largest proportion of loss in the HP. Therefore increasing the understanding of such flows will allow for improvements in design of such compressors, increasing efficiency, stability, and the operating range. Experimental and computational techniques have...
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Publication status:: Published

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APA Style

Williams, R., Gregory-Smith, D., He, L., & Ingram, G. (2010). Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade. 132(2), 021018–021018.

MLA Style

Williams, R., et al. Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade. no. 2, 2010, pp. 021018–18.

Chicago Style

Williams, R, D Gregory-Smith, L He, and G Ingram. 2010. “Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade.” In , 132:021018–18.
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Publisher copy:: 10.1115/1.3104611

Authors

+ Williams, R More by this author

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Author

+ Gregory-Smith, D More by this author

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+ He, L More by this author

Institution:

University of Oxford

Division:

MPLS

Department:

Engineering Science

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+ Ingram, G More by this author

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Bibliographic Details

Host title:: JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Volume:: 132
Issue:: 2
Pages:: 021018-021018
Publication date:: 2010-04-01
DOI:: 10.1115/1.3104611
EISSN:: 1528-8900
ISSN:: 0889-504X

Item Description

Keywords:: jets

compressors

gas turbines

blades
Pubs id:: pubs:62177
UUID:: uuid:2db7e3b6-510b-4527-940e-36c31f67320d
Local pid:: pubs:62177
Source identifiers:: 62177
Deposit date:: 2013-11-16

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Copyright date:: 2010

Licence:: Terms and Conditions of Use for Oxford University Research Archive

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