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1
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Simulation of Three-Dimensional Viscous Flow Within a Multi-stage Turbine
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Adamczyk, J. J., Celestina, M. L., Beach, T. A., and Barnett, M., 1989, “Simulation of Three-Dimensional Viscous Flow Within a Multi-stage Turbine,” ASME Journal of Turbomachinery, Vol. 112, pp. 370-376.
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Adamczyk, J.J.1
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2
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The Role of Tip Clearance in High-Speed Fan Stall
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Adamczyk, J. J., Celestina, M. L., and Greitzer, E. M., 1993, “The Role of Tip Clearance in High-Speed Fan Stall,” ASME Journal of Turbomachinery, Vol. 115, pp. 28-38.
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Adamczyk, J.J.1
Celestina, M.L.2
Greitzer, E.M.3
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3
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0026138972
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Similarity Analysis of Tip Clearance Flow Structure
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Chen, G. T., Greitzer, E. M., Tan, C. S., and Marble, F. E., 1991, “Similarity Analysis of Tip Clearance Flow Structure,” ASME Journal of Turbomachinery, Vol. 113, pp. 260-271.
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Chen, G.T.1
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Tan, C.S.3
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4
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85006956512
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Three-Dimensional Flow Phenomena in a Transonic, High-Throughflow, Axial-Flow Compressor Stage
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Copenhaver, W. W., Hah, C., and Puterbaugh, S. L., 1993, “Three-Dimensional Flow Phenomena in a Transonic, High-Throughflow, Axial-Flow Compressor Stage,” ASME Journal of Turbomachinery, Vol. 115, pp. 240-248.
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Copenhaver, W.W.1
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Puterbaugh, S.L.3
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5
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Numerical Investigation of Endwall/Casing Treatment Flow Phenomena
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Cambridge, MA
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Crook, A.1
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6
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0027624887
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Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field
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Hathaway, M. D., Chriss, R. M., Wood, J. R., and Strazisar, A. J., 1993, “Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field,” ASME Journal of Turbomachinery, Vol. 115, pp. 527-542.
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Hathaway, M.D.1
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7
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Behavior of Tip Leakage Flow Behind an Axial Compressor Rotor
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Inoue, M., Kuroumaru, M., and Fukuhara, M., 1986, “Behavior of Tip Leakage Flow Behind an Axial Compressor Rotor,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 108, pp. 7-13.
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Inoue, M.1
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8
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0024702584
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Structure of Tip Clearance Flow in an Isolated Axial Compressor Rotor
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Inoue, M., and Kuroumaru, M., 1989, “Structure of Tip Clearance Flow in an Isolated Axial Compressor Rotor,” ASME Journal of Turbomachinery, Vol. III, pp. 250-256.
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Inoue, M.1
Kuroumaru, M.2
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9
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0346577937
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Paper No. AIAA-90-2356
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Kirtley, K. R., Beach, T. A., and Adamczyk, J. J., 1990, “Numerical Analysis of Secondary Flow in a Two-Stage Turbine,” Paper No. AIAA-90-2356.
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Numerical Analysis of Secondary Flow in a Two-Stage Turbine
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Kirtley, K.R.1
Beach, T.A.2
Adamczyk, J.J.3
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10
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0025136356
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Stall Inception in Axial Compressors
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McDougall, N. M., Cumpsty, N. A., and Hynes, T. P., 1990, “Stall Inception in Axial Compressors,” ASME Journal of Turbomachinery, Vol. 112, pp. 116-125.
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McDougall, N.M.1
Cumpsty, N.A.2
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11
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0025208685
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A Comparison Between the Design Point and Near Stall Performance of an Axial Compressor
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McDougall, N. M., 1990, “A Comparison Between the Design Point and Near Stall Performance of an Axial Compressor,” ASME Journal of Turbomachinery, Vol. 112, pp. 109-115.
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McDougall, N.M.1
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12
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1542370443
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Performance of Single-Stage Axial-Flow Transonic Compressor With Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio of 2.05
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Moore, R. D., and Reid, L., 1980, “Performance of Single-Stage Axial-Flow Transonic Compressor With Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio of 2.05,” NASA TP 1659.
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Moore, R.D.1
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13
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Preparation of Polystyrene Microspheres for Laser Velocimetry in Wind Tunnels
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Nichols, C. E., Jr., 1987, “Preparation of Polystyrene Microspheres for Laser Velocimetry in Wind Tunnels,” NASA TM 89163.
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Nichols, C.E.1
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14
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0009262616
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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., and Moore, R. D., 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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Reid, L.1
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15
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0027624888
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Measurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor
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Stauter, R. C., 1993, “Measurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor,” ASME Journal of Turbomachinery, Vol. 115, pp. 468-476.
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ASME Journal of Turbomachinery
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Stauter, R.C.1
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16
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0028179332
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An Approximate Analysis and Prediction Method for Tip Clearance Loss in Axial Compressors
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Storer, J. A., and Cumpsty, N. A., 1994, “An Approximate Analysis and Prediction Method for Tip Clearance Loss in Axial Compressors,” ASME Journal of Turbomachinery, Vol. 116, pp. 648-656.
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Storer, J.A.1
Cumpsty, N.A.2
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17
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0003210886
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Laser Anemometer Measurements in a Transonic Axial-Flow Fan Rotor
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Strazisar, A.J.1
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18
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85025182852
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Performance of Tandem-Bladed Transonic Compressor Rotor With Rotor Tip Speed of 1375 Feet per Second
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Urasek, D. C., and Janetzke, D. C., 1972, “Performance of Tandem-Bladed Transonic Compressor Rotor With Rotor Tip Speed of 1375 Feet per Second,” NASA TM X-2484.
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Urasek, D.C.1
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19
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0022045543
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Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing
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Wisler, D. C., 1985, “Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing,” ASME Journal of Turbomachinery, Vol. 107, pp. 354-363.
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Wisler, D.C.1
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