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Volumn 5 B, Issue , 2002, Pages 1141-1153

Application of casing circumferential grooves for improved stall margin in a transonic axial compressor

Author keywords

[No Author keywords available]

Indexed keywords

CASING CIRCUMFERENTIAL GROOVES; ENDWALL BOUNDARY LAYER THICKNESS; TRANSONIC AXIAL COMPRESSOR;

EID: 0037003646     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30641     Document Type: Conference Paper
Times cited : (83)

References (16)
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  • 2
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  • 3
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    • A study of configurations of casing treatment for axial flow compressors
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    • (1985) Bull. of JSME , vol.27 , Issue.230 , pp. 1675-1681
    • Fujita, H.1    Takata, H.2
  • 4
    • 84885299431 scopus 로고
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    • ASME Paper 94-Gt-99
    • Gorrel, S.E. and Russler, P.M., 1994, "Stall Inception in a High-Speed Low Aspect Ratio Fan Including the Effects of Casing Treatments," ASME Paper 94-Gt-99.
    • (1994)
    • Gorrel, S.E.1    Russler, P.M.2
  • 5
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    • (2001)
    • Hah, C.1    Rabe, D.C.2
  • 6
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    • Hah, C. and Wennerstrom, A.J., 1990, "Three-Dimensional Flow Fields Inside a Transonic Compressor with Swept Blades," ASME Journal of Turbomachinery, Vol. 113, No. 1, pp. 241-251.
    • (1990) ASME Journal of Turbomachinery , vol.113 , Issue.1 , pp. 241-251
    • Hah, C.1    Wennerstrom, A.J.2
  • 7
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    • (1996)
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  • 8
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  • 9
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  • 10
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    • Effect of casing treatment on overall and blade-element performance of a compressor rotor
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  • 11
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    • (1982)
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  • 12
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  • 13
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  • 15
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  • 16
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    • (1997)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.