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Volumn 112, Issue 4, 1990, Pages 679-687

Three-dimensional separated flow field in the endwall region of an annular compressor cascade in the presence of rotor-stator interaction: Part 2-unsteady flow and pressure field

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[No Author keywords available]

Indexed keywords


EID: 0141945561     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2927708     Document Type: Article
Times cited : (22)

References (24)
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    • Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 1—QuasiSteady Flow Field and Comparison With Steady-State Date
    • this issue
    • Schulz, H. D., Gallus, H.E., and Lakshminarayana, B., 1990, “Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 1—QuasiSteady Flow Field and Comparison With Steady-State Date,” ASME Journal of Turbomachinery, Vol. 112, this issue.
    • (1990) ASME Journal of Turbomachinery , vol.112
    • Schulz, H.D.1    Gallus, H.E.2    Lakshminarayana, B.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.