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Volumn 33, Issue 6, 2002, Pages 899-908

DPIV study of near-stall wake-rotor interactions in a transonic compressor

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; DIGITAL INSTRUMENTS; FLOW VISUALIZATION; ROTORS; STATISTICAL METHODS; SYSTEMS ANALYSIS; VELOCITY MEASUREMENT; WAKES;

EID: 0036922019     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-002-0503-y     Document Type: Article
Times cited : (15)

References (18)
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  • 2
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    • (2000) ASME J Turbomach , vol.122 , pp. 743-750
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  • 3
    • 0028025839 scopus 로고
    • Detailed flow measurement and predictions for a three-stage transonic fan
    • Calvert WJ (1994) Detailed flow measurement and predictions for a three-stage transonic fan. ASME J Turbomach 116:298-305
    • (1994) ASME J Turbomach , vol.116 , pp. 298-305
    • Calvert, W.J.1
  • 4
    • 0003987201 scopus 로고
    • Design and test of a low aspect ratio fan stage
    • AIAA Paper No. 88-2816m AIAA, Reston, Va.
    • Creason T, Baghdadi S (1988) Design and test of a low aspect ratio fan stage. AIAA Paper No. 88-2816, AIAA, Reston, Va.
    • (1988)
    • Creason, T.1    Baghdadi, S.2
  • 5
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    • High-resolution measurements of two-dimensional instabilities and turbulence transition in plane mixing layers
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    • Estevadeordal, J.1    Kleis, S.2
  • 8
    • 0000790012 scopus 로고    scopus 로고
    • Study of wake-blade interactions in a transonic compressor using flow visualization and DPIV
    • Estevadeordal J, Gogineni S, Goss L, Copenhaver W, Gorrell S (2002) Study of wake-blade interactions in a transonic compressor using flow visualization and DPIV. J Fluids Eng 124:166-175
    • (2002) J Fluids Eng , vol.124 , pp. 166-175
    • Estevadeordal, J.1    Gogineni, S.2    Goss, L.3    Copenhaver, W.4    Gorrell, S.5
  • 9
    • 0034845629 scopus 로고    scopus 로고
    • Upstream wake influences on the measured performance of a transonic compressor stage
    • Gorrell S, Copenhaver W, Chriss R (2001) Upstream wake influences on the measured performance of a transonic compressor stage. J Propul Power 17:43-48
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  • 10
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    • (2002) ASME TURBO EXPO 2002, 3-6 June 2002, Amsterdam, the Netherlands
    • Gorrell, S.1    Okiishi, T.2    Copenhaver, W.3
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.