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Volumn 120, Issue 3, 1998, Pages 465-476

Blockage development in a transonic, axial compressor rotor

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYER FLOW; FLOW MEASUREMENT; INTAKE SYSTEMS; LASER APPLICATIONS; ROTORS; TRANSONIC FLOW;

EID: 0032125009     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841741     Document Type: Article
Times cited : (111)

References (27)
  • 2
    • 0024858972 scopus 로고
    • Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
    • Adamczyk, J., Celestina, M., Beach, T., and Barnett, M., 1989, “Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine,” ASME Journal of Turbo machinery, Vol. 112, pp. 370-376.
    • (1989) ASME Journal of Turbo Machinery , vol.112 , pp. 370-376
    • Adamczyk, J.1    Celestina, M.2    Beach, T.3    Barnett, M.4
  • 3
    • 0015627976 scopus 로고
    • An Experimental Investigation of Turbulent Transonic Viscious-In viscid Interactions
    • Alber, I., Bacon, J., Masson, B., 1973, “An Experimental Investigation of Turbulent Transonic Viscious-In viscid Interactions,” AIAA Journal, Vol. 11, No. 5, pp. 620-627.
    • (1973) AIAA Journal , vol.11 , Issue.5 , pp. 620-627
    • Alber, I.1    Bacon, J.2    Masson, B.3
  • 4
    • 0026627107 scopus 로고
    • A Study of the Interaction of a Normal Shock Wave With a Turbulent Boundary Layer at Mach Numbers Between 1.3 and 1.5
    • Atkin, C., and Squire, L., 1992, “A Study of the Interaction of a Normal Shock Wave With a Turbulent Boundary Layer at Mach Numbers Between 1.3 and 1.5,” European Journal Mechanics B/Fluids, Vol. 11, No. 1.
    • (1992) European Journal Mechanics B/Fluids , vol.11 , Issue.1
    • Atkin, C.1    Squire, L.2
  • 6
    • 0031921967 scopus 로고    scopus 로고
    • Calculation of Tip Clearance Effects in a Transonic Compressor Rotor
    • Also NASA TM 107216
    • Chima, R., 1998, “Calculation of Tip Clearance Effects in a Transonic Compressor Rotor,” ASME Journal of Turbo machinery, Vol. 120, pp. 131-140; Also NASA TM 107216.
    • (1998) ASME Journal of Turbo Machinery , vol.120 , pp. 131-140
    • Chima, R.1
  • 11
    • 0004299307 scopus 로고
    • The Effects of Tip Clearance on Axial Compressor Pressure Rise
    • Ph.D. Dissertation
    • Khalid, S., 1994, “The Effects of Tip Clearance on Axial Compressor Pressure Rise,” Ph.D. Dissertation, Massachusetts Institute of Technology.
    • (1994) Massachusetts Institute of Technology
    • Khalid, S.1
  • 12
    • 0019622405 scopus 로고
    • Stalling Pressure Rise Capability of Axial Flow Compressor Stages, ASME
    • Koch, C., 1981, “Stalling Pressure Rise Capability of Axial Flow Compressor Stages,” ASME Journal of Engineering for Power, Vol. 103, pp. 645-656.
    • (1981) Journal of Engineering for Power , vol.103 , pp. 645-656
    • Koch, C.1
  • 13
    • 0016973006 scopus 로고
    • Loss Sources and Magnitudes in Axial-Flow Compressors, ASME
    • Koch, C., and Smith, L., 1976, “Loss Sources and Magnitudes in Axial-Flow Compressors,” ASME Journal of Engineering for Power, Vol. 98, pp. 411-424.
    • (1976) Journal of Engineering for Power , vol.98 , pp. 411-424
    • Koch, C.1    Smith, L.2
  • 14
    • 0000614687 scopus 로고
    • The Interaction Between Boundary Layer and Shock Waves in Transonic Flow
    • Liepmann, H., 1946, “The Interaction Between Boundary Layer and Shock Waves in Transonic Flow,” Journal of Aeron. Sciences, Vol. 13, No. 12.
    • (1946) Journal of Aeron. Sciences , vol.13 , Issue.12
    • Liepmann, H.1
  • 20
    • 33646413620 scopus 로고
    • Flow Produced by Interaction of a Turbulent Boundary Layer With a Normal Shock Wave of Strength Sufficient to Cause Separation
    • Seddon, J., 1960, “Flow Produced by Interaction of a Turbulent Boundary Layer With a Normal Shock Wave of Strength Sufficient to Cause Separation,” Brit. Aero. Res. Council Report and Memo No. 3502.
    • (1960) Brit. Aero. Res. Council Report and Memo No. 3502
    • Seddon, J.1
  • 22
    • 0002639026 scopus 로고
    • Casing Boundary Layers in Multistage Axial-Flow Compressors
    • A. L. S. Dzung, ed., Elsevier
    • Smith, J. L. H., 1970, “Casing Boundary Layers in Multistage Axial-Flow Compressors,” Flow Research on Blading, A. L. S. Dzung, ed., Elsevier, pp. 275-304.
    • (1970) Flow Research on Blading , pp. 275-304
    • Smith, J.L.H.1
  • 24
    • 0029674548 scopus 로고    scopus 로고
    • Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor
    • Suder, K., and Celestina, M., 1996, “Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor,” ASME Journal of Turbo machinery, Vol. 118, pp. 218-229
    • (1996) ASME Journal of Turbo Machinery , vol.118 , pp. 218-229
    • Suder, K.1    Celestina, M.2
  • 25
    • 0013432968 scopus 로고    scopus 로고
    • Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor With Respect to the Development of Blockage and Loss
    • Ph.D. Dissertation
    • Suder, K. L., 1996, “Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor With Respect to the Development of Blockage and Loss,” Ph.D. Dissertation, Case Western Reserve University: also NASA TM 107310.
    • (1996) Case Western Reserve University: Also NASA TM 107310
    • Suder, K.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.