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Volumn 125, Issue 1, 2003, Pages 133-140

Evolution of upstream propagating shock waves from a transonic compressor rotor

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPRESSORS; COMPUTER SIMULATION; SHOCK WAVES; TRANSONIC FLOW; TURBOMACHINE BLADES; VISCOSITY;

EID: 0037852063     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1516813     Document Type: Article
Times cited : (25)

References (22)
  • 2
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    • Variations in upstream vane loading with changes in back pressure in a transonic compressor
    • Probasco, D. P., Leger, T. J., Wolff, J. M., Copenhaver, W. W., and Chriss, R., 2000, "Variations in Upstream Vane Loading with Changes in Back Pressure in a Transonic Compressor," ASME J. Turbomach., 122, pp. 433-441.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 433-441
    • Probasco, D.P.1    Leger, T.J.2    Wolff, J.M.3    Copenhaver, W.W.4    Chriss, R.5
  • 3
    • 0025544847 scopus 로고
    • Non-reflecting boundary conditions for Euler equation calculations
    • Giles, M. B., 1988. "Non-Reflecting Boundary Conditions for Euler Equation Calculations," AIAA J., 28, pp. 2050-2058.
    • (1988) AIAA J. , vol.28 , pp. 2050-2058
    • Giles, M.B.1
  • 4
    • 85069385330 scopus 로고
    • Intra-stator transport of rotor wakes and its effect on compressor performance
    • Kerrebrock, J. L., and Mikolajczak, A. A., 1970, "Intra-stator Transport of Rotor Wakes and its Effect on Compressor Performance," ASME J. Eng. Power, 92, pp. 359-368.
    • (1970) ASME J. Eng. Power , vol.92 , pp. 359-368
    • Kerrebrock, J.L.1    Mikolajczak, A.A.2
  • 5
    • 0020209106 scopus 로고
    • A multiple-grid scheme for solving Euler equations
    • Ni, R.-H., 1982, "A Multiple-Grid Scheme for Solving Euler Equations," AIAA J., 20, pp. 1565-1571.
    • (1982) AIAA J. , vol.20 , pp. 1565-1571
    • Ni, R.-H.1
  • 11
    • 0014808828 scopus 로고
    • Shock-wave radiation from a supersonic ducted rotor
    • Royal Aeronautical Society
    • Morfey, C. L., and Fisher, M. J., 1970, "Shock-wave Radiation from a Supersonic Ducted Rotor," Aeronaut. J., Royal Aeronautical Society, 74, pp. 579-585.
    • (1970) Aeronaut. J. , vol.74 , pp. 579-585
    • Morfey, C.L.1    Fisher, M.J.2
  • 12
    • 0013377595 scopus 로고
    • On the attenuation of a repeated Sawtooth shock wave
    • Rudnick, I., 1953, "On the Attenuation of a Repeated Sawtooth Shock Wave," J. Acoust. Soc. Am., 25, pp. 1012-1013.
    • (1953) J. Acoust. Soc. Am. , vol.25 , pp. 1012-1013
    • Rudnick, I.1
  • 13
    • 0025156446 scopus 로고
    • Throughflow theory for nonaxisymmetric turbomachinery flow - Part I: Formulation
    • Dring, R. P., and Oates, G. C., 1990. "Throughflow Theory for Nonaxisymmetric Turbomachinery Flow-Part I: Formulation," ASME J. Turbomach., 112, pp. 320-327.
    • (1990) ASME J. Turbomach. , vol.112 , pp. 320-327
    • Dring, R.P.1    Oates, G.C.2
  • 14
    • 0034541762 scopus 로고    scopus 로고
    • Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors
    • van Zante, D. E., Strasizar, A. J., Hathaway, M. D., and Okiishi, T. H. 2000. "Recommendations for Achieving Accurate Numerical Simulation of Tip Clearance Flows in Transonic Compressor Rotors," ASME J. Turbomach., 122, pp. 733-742.
    • (2000) ASME J. Turbomach. , vol.122 , pp. 733-742
    • van Zante, D.E.1    Strasizar, A.J.2    Hathaway, M.D.3    Okiishi, T.H.4
  • 15
    • 0013331995 scopus 로고
    • Flow in cascades with a transonic regime
    • ed., L. S. Dzung, Elsevier
    • Chauvin, J., Sieverding, C., and Griepentrog, H., 1970, "Flow in Cascades with a Transonic Regime," Flow Research on Blading, ed., L. S. Dzung, pp. 151-189, Elsevier.
    • (1970) Flow Research on Blading , pp. 151-189
    • Chauvin, J.1    Sieverding, C.2    Griepentrog, H.3
  • 16
    • 0013376031 scopus 로고    scopus 로고
    • Impact of unsteadiness induced by adjacent airfoil rows on the performance, structural integrity and stalling characteristics of axial flow compressors
    • von Karman Institute
    • Sharma, O. P., and Tan, C. S., 1999, "Impact of Unsteadiness Induced by Adjacent Airfoil Rows on the Performance, Structural Integrity and Stalling Characteristics of Axial Flow Compressors," Blade Interference Effects in Axial Turbomachinery Stages, von Karman Institute.
    • (1999) Blade Interference Effects in Axial Turbomachinery Stages
    • Sharma, O.P.1    Tan, C.S.2
  • 17
    • 0002639026 scopus 로고
    • Casing boundary layers in multistage axial-flow compressors
    • ed., L. S. Dzung, Elsevier
    • Smith, L. H., 1970, "Casing Boundary Layers in Multistage Axial-flow Compressors," Flow Research on Blading, ed., L. S. Dzung, 275-304, Elsevier.
    • (1970) Flow Research on Blading , pp. 275-304
    • Smith, L.H.1
  • 21
    • 0035279060 scopus 로고    scopus 로고
    • Transonic compressor influences on upstream surface pressures with axial spacing
    • Koch, P. J., Probasco, D. P., Wolff, J. M., Copenhaver, W. W., and Chriss, R., 2000, "Transonic Compressor Influences on Upstream Surface Pressures with Axial Spacing," J. Propul. Power, 117, pp. 474-476.
    • (2000) J. Propul. Power , vol.117 , pp. 474-476
    • Koch, P.J.1    Probasco, D.P.2    Wolff, J.M.3    Copenhaver, W.W.4    Chriss, R.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.