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Volumn 1, Issue , 1998, Pages

Flow measurement in a multistage large scale low speed axial flow research compressor

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW; AXIAL-FLOW COMPRESSORS; COMPRESSORS; DATA ACQUISITION; FLOW MEASUREMENT; FLOWMETERS; GAS TURBINES; NAVIER STOKES EQUATIONS;

EID: 84971511343     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-432     Document Type: Conference Paper
Times cited : (19)

References (5)
  • 1
    • 0022045543 scopus 로고
    • Loss reduction in axial-row compressors through low-speed model testing
    • Wisler, D. C., 1985, 'Loss Reduction in Axial-Row Compressors Through Low-Speed Model Testing', ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 354-363
    • (1985) ASME Journal of Engineering for Gas Turbines and Power , vol.107 , pp. 354-363
    • Wisler, D.C.1
  • 2
    • 0028525732 scopus 로고
    • Endwall effects at two tip clearances in a multistage axial row compressor with controlled diffusion blading
    • Howard M. A., Ivey P. C., Barton J. P., Young K. F., 1994, 'Endwall Effects at Two Tip Clearances in a Multistage Axial Row Compressor with Controlled Diffusion Blading', ASME Journal of Turbomachinery, Vol. 116, pp. 635-647
    • (1994) ASME Journal of Turbomachinery , vol.116 , pp. 635-647
    • Howard, M.A.1    Ivey, P.C.2    Barton, J.P.3    Young, K.F.4
  • 3
    • 84970882201 scopus 로고
    • Through-row analysis of a multistage compressor: Part I - Aerodynamic input; Part II - Analytical-experimental comparisons
    • Dring, R. P. and Joslyn, H. D., 1986, 'Through-Row Analysis of a Multistage Compressor: Part I - Aerodynamic Input; Part II - Analytical-Experimental Comparisons', ASME Journal of Turbomachinery, Vol. 108, pp. 17-31
    • (1986) ASME Journal of Turbomachinery , vol.108 , pp. 17-31
    • Dring, R.P.1    Joslyn, H.D.2
  • 5
    • 84971508863 scopus 로고    scopus 로고
    • Three-dimensional separated row field in the endwall region of an annular compressor cascade in the presence of rotor-stator interaction - Part I: Quasi-steady row field and comparison with steady-state data
    • Schulz, H. D., Gallus, H. E., Lakshminarayana, B., 'Three-Dimensional Separated Row Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction - Part I: Quasi-Steady Row Field and Comparison with Steady-State Data', ASME Paper No. 89-GT-76
    • ASME Paper
    • Schulz, H.D.1    Gallus, H.E.2    Lakshminarayana, B.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.