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An Inviscid-Viscous Interaction Treatment to Predict the Blade-to-Blade Performance of Axial Compressors with Leading Edge Normal Shock Waves
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Calvert W. J., 1982, “An Inviscid-Viscous Interaction Treatment to Predict the Blade-to-Blade Performance of Axial Compressors with Leading Edge Normal Shock Waves,” ASME Paper 82-GT-135
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ASME Paper 82-GT-135
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Calvert, W.J.1
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2
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84939185472
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An Off-Design Loss and Deviation Prediction Study for Transonic Axial Compressors
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Cetin M., Hirsch Ch., Serovy G. K., and Ucer A. S., 1989, “An Off-Design Loss and Deviation Prediction Study for Transonic Axial Compressors,” ASME Paper 89-GT-324
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ASME Paper 89-GT-324
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Cetin, M.1
Hirsch, C.H.2
Serovy, G.K.3
Ucer, A.S.4
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3
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Development of a 3D Navier-Stokes Solver for Application to All Types of Turbomachinery,’
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Dawes W. N., 1988, “Development of a 3D Navier-Stokes Solver for Application to All Types of Turbomachinery,” ASME Paper 88-GT-70
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ASME Paper 88-GT-70
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Dawes, W.N.1
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4
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85011671649
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Conceptionet Essais d’un Etage de Tete d’un Compresseur HP Avance
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Advanced Technology for Aero Gas Turbine Components, Paris
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Goutines, M.1
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0025212015
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Three-Dimensional Flowfields Inside a Transonic Compressor with Swept Blades
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Hah C., and Wennerstrom A. J., 1990, “Three-Dimensional Flowfields Inside a Transonic Compressor with Swept Blades,” ASME Paper 90-GT-359
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(1990)
ASME Paper 90-GT-359
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Hah, C.1
Wennerstrom, A.J.2
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6
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0016993770
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Analytical theory of transonic normal shock-boundary layer interaction
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A Secondary Flow Calculation Method for One Stage Axial Transonic Flow Compressors, Including Shock-Secondary Flow Interaction
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Kaldellis J., Douvikas D., Falchetti F., Papailiou K., 1990, “A Secondary Flow Calculation Method for One Stage Axial Transonic Flow Compressors, Including Shock-Secondary Flow Interaction,” ASME Journal of Turbomachinery, Vol. 112, pp. 652-668
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Kaldellis, J.1
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Parametrical Investigation of the Interaction Between Tur-bulent Wall Shear Layers and Normal Shock Waves, Including Separation
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Kaldellis J., 1993, “Parametrical Investigation of the Interaction Between Tur-bulent Wall Shear Layers and Normal Shock Waves, Including Separation,” ASME JOURNAL OF FLUIDS ENGINEERING, Vol. 115, pp. 48-55
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, vol.115
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Kaldellis, J.1
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Energy Exchange and Loss Prediction in Axial Turbines and Compressors
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Firenze, Italy
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Kaldellis, J., 1994, “Energy Exchange and Loss Prediction in Axial Turbines and Compressors,” presented at the FLOWERS’94 ASME Conference, Confer-ence Proceeding pp. 799-811, Firenze, Italy
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Kaldellis, J.1
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11
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0023827505
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Design of High Performance Fans Using Advanced Aerodynamic Codes
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Karadimas G., 1988, “Design of High Performance Fans Using Advanced Aerodynamic Codes,” ASME Paper 88-GT-141
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ASME Paper 88-GT-141
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Karadimas, G.1
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12
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0025797927
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3-D Loss Prediction Based on Secondary Flow and Blade Shear Layer Interaction
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Katramatos D., and Kaldellis J., 1991, “3-D Loss Prediction Based on Secondary Flow and Blade Shear Layer Interaction,” ASME Paper 91-GT-59
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ASME Paper 91-GT-59
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Katramatos, D.1
Kaldellis, J.2
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13
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84991617387
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Loss Sources and Magnitudes in Axial Flow Compressors
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Koch C., and Smith Jr. L. H., 1976, “Loss Sources and Magnitudes in Axial Flow Compressors,” Trans. of ASME, Journal of Engineering for Power, Vol. 98, pp. 411-424
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Koch, C.1
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The Flow Produced by Interaction of a Turbulent Boundary Layer with a Normal Shock Wave of Strength Sufficient to Cause Separation
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Laser Two-Focus Anemometry Inves-tigation of the Flow Field Within a Supersonic Axial Compressor Rotor
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Trebinjac I., and Vouillarmet A., 1990, “Laser Two-Focus Anemometry Inves-tigation of the Flow Field Within a Supersonic Axial Compressor Rotor,” ASME Paper 90-GT-298
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ASME Paper 90-GT-298
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Trebinjac, I.1
Vouillarmet, A.2
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18
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Experimental Investigation of the Performance of a Supersonic Compressor Cascade
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Tweedt T. L., Schreiber H. A., and Starken H., 1988, “Experimental Investigation of the Performance of a Supersonic Compressor Cascade,” ASME Paper 88-GT-306
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ASME Paper 88-GT-306
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Tweedt, T.L.1
Schreiber, H.A.2
Starken, H.3
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