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Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
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Adamczyk, J.1
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An Experimental Investigation of Turbulent Transonic Viscious-In viscid Interactions
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A Study of the Interaction of a Normal Shock Wave With a Turbulent Boundary Layer at Mach Numbers Between 1.3 and 1.5
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Atkin, C.1
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0031921967
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Calculation of Tip Clearance Effects in a Transonic Compressor Rotor
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Also NASA TM 107216
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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.
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Chima, R.1
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7
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3643077803
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Paper No. AIAA-87-1369
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Shock Wave Boundary Layer Interaction in Cascades
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J. Surugue, ed
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Griepentrog, H., 1972, “Shock Wave Boundary Layer Interaction in Cascades,” AGARDograph No. 164, Boundary Layer Effects in Turbo machines, J. Surugue, ed., pp. 443-456.
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Griepentrog, H.1
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The Effects of Tip Clearance on Axial Compressor Pressure Rise
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Ph.D. Dissertation
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12
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0019622405
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Stalling Pressure Rise Capability of Axial Flow Compressor Stages, ASME
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Journal of Engineering for Power
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Koch, C.1
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0016973006
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Loss Sources and Magnitudes in Axial-Flow Compressors, ASME
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14
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The Interaction Between Boundary Layer and Shock Waves in Transonic Flow
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Moore, R.1
Reid, L.2
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18
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Reid, L., and Moore, R., 1978, “Design and Overall Performance of Four Highly Loaded, High-Speed Inlet Stages for an Advanced High-Pressure Ratio Core Compressor,” NASA TP 1337.
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Design and Overall Performance of Four Highly Loaded, High-Speed Inlet Stages for an Advanced High-Pressure Ratio Core Compressor
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Reid, L.1
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Flow Produced by Interaction of a Turbulent Boundary Layer With a Normal Shock Wave of Strength Sufficient to Cause Separation
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Shabbir, A., Zhu, J., and Celestina, M., 1996, “Assessment of Three Turbulence Models in a Compressor Rotor,” ASME Paper No. 96-GT-198.
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Assessment of Three Turbulence Models in a Compressor Rotor
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Casing Boundary Layers in Multistage Axial-Flow Compressors
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Laser Anemometer Measurements in a Transonic Axial-Flow Fan Rotor
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Strazisar, A.1
Wood, J.2
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24
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0029674548
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Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor
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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
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Suder, K.1
Celestina, M.2
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25
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Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor With Respect to the Development of Blockage and Loss
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Ph.D. Dissertation
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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.
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Suder, K.L.1
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27
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Shock Structure Measured in a Transonic Fan Using Laser Anemometry
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Wood, J., Strazisar, A., and Simonyi, P., 1986, “Shock Structure Measured in a Transonic Fan Using Laser Anemometry,” AGARD CP-401: Transonic and Supersonic Phenomena in Turbo machines.
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AGARD CP-401: Transonic and Supersonic Phenomena in Turbo Machines
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