-
2
-
-
0141443691
-
Casing boundary layers in multistage compressors
-
Dzung, L. S., ed.
-
Smith, L. H., Jr, 1969, "Casing Boundary Layers in Multistage Compressors," Proc. Symp. Flow Research on Blading, Dzung, L. S., ed.
-
(1969)
Proc. Symp. Flow Research on Blading
-
-
Smith L.H., Jr.1
-
3
-
-
0343667728
-
Axial-flow turbomachine through flow calculation methods
-
Ch. Hirsch and J. D. Denton, eds.
-
Serovy, G. K., 1981, "Axial-Flow Turbomachine Through Flow Calculation Methods," AGARD Advisory Report No. 175, Through Flow Calculations in Axial Turbomachines, Ch. Hirsch and J. D. Denton, eds.
-
(1981)
AGARD Advisory Report No. 175, Through Flow Calculations in Axial Turbomachines
, vol.175
-
-
Serovy, G.K.1
-
4
-
-
0003747148
-
-
Longman Scientific & Technical, Publisher
-
Cumpsty, N. A., 1989, Compressor Aerodynamics, Longman Scientific & Technical, Publisher.
-
(1989)
Compressor Aerodynamics
-
-
Cumpsty, N.A.1
-
6
-
-
0022698712
-
The importance of circumferential non-uniformities in a passage-averaged quasi-three-dimensional turbomachinery design system
-
Jennions, I. K., and Stow, P., 1986, "The Importance of Circumferential Non-uniformities in a Passage-Averaged Quasi-Three-Dimensional Turbomachinery Design System," ASME J. Eng. Gas Turbines Power, 108, pp. 240-245.
-
(1986)
ASME J. Eng. Gas Turbines Power
, vol.108
, pp. 240-245
-
-
Jennions, I.K.1
Stow, P.2
-
7
-
-
0027441351
-
Viscous throughflow modeling for multi-stage compressor design
-
Howard, M. A., and Gallimore, S. J., 1993, "Viscous Throughflow Modeling for Multi-Stage Compressor Design," ASME J. Turbomach., 115, p. 296.
-
(1993)
ASME J. Turbomach.
, vol.115
, pp. 296
-
-
Howard, M.A.1
Gallimore, S.J.2
-
8
-
-
0032194746
-
Viscous throughflow modeling of axial compressor bladerows using a tangential blade force hypothesis
-
Gallimore, S. J., 1998a, "Viscous Throughflow Modeling of Axial Compressor Bladerows Using a Tangential Blade Force Hypothesis," ASME J. Turbomach., 120, p. 662.
-
(1998)
ASME J. Turbomach.
, vol.120
, pp. 662
-
-
Gallimore, S.J.1
-
9
-
-
0032754715
-
Endwall blockage in axial compressors
-
Khalid, S. A., Khalsa, A. S., Waitz, I. A., Tan, C. S., Greitzer, E. M., Cumpsty, N. A., Adamczyk, J. J., and Marble, F. E., 1999, "Endwall Blockage in Axial Compressors," ASME J. Turbomach., 121, pp. 499-509.
-
(1999)
ASME J. Turbomach.
, vol.121
, pp. 499-509
-
-
Khalid, S.A.1
Khalsa, A.S.2
Waitz, I.A.3
Tan, C.S.4
Greitzer, E.M.5
Cumpsty, N.A.6
Adamczyk, J.J.7
Marble, F.E.8
-
10
-
-
84890131308
-
-
ASME Paper No. 99-GT-390, accepted for the ASME J. Turbomachinery
-
Van Zante, D. E., Strazisar, A. J., Wood, J. R., Hathaway, M. D., and Okiishi, T. H., 1999, "Recommendations for Achieving Accurate Numerical Simulation of Tip Clearance Flow in Transonic Compressor Rotors," ASME Paper No. 99-GT-390, accepted for the ASME J. Turbomachinery.
-
(1999)
Recommendations for Achieving Accurate Numerical Simulation of Tip Clearance Flow in Transonic Compressor Rotors
-
-
Van Zante, D.E.1
Strazisar, A.J.2
Wood, J.R.3
Hathaway, M.D.4
Okiishi, T.H.5
-
11
-
-
0034106609
-
Modeling shrouded stator cavity flows in axial-flow compressors
-
Wellborn, S. R., Tolchinsky, I., and Okiishi, T. H., 2000, "Modeling Shrouded Stator Cavity Flows in Axial-Flow Compressors," ASME J. Turbomach., 122, pp. 55-61.
-
(2000)
ASME J. Turbomach.
, vol.122
, pp. 55-61
-
-
Wellborn, S.R.1
Tolchinsky, I.2
Okiishi, T.H.3
-
12
-
-
0003548692
-
-
VKI-LEC-SER-1979-7, VKI
-
Denton, J. D., and Singh, U. K., 1979, "Time Marching Methods for Turbomachinery Flow Calculations," VKI-LEC-SER-1979-7, VKI.
-
(1979)
Time Marching Methods for Turbomachinery Flow Calculations
-
-
Denton, J.D.1
Singh, U.K.2
-
13
-
-
0026715368
-
Toward improved throughflow capability: The use of three-dimensional viscous flow solvers in a multistage environment
-
Dawes, W. N., 1992, "Toward Improved Throughflow Capability: The Use of Three-Dimensional Viscous Flow Solvers in a Multistage Environment," ASME J. Turbomach., 114, pp. 8-17.
-
(1992)
ASME J. Turbomach.
, vol.114
, pp. 8-17
-
-
Dawes, W.N.1
-
14
-
-
0026765731
-
The calculation of three-dimensional viscous flow through multistage turbomachines
-
Denton, J. D., 1992, "The Calculation of Three-Dimensional Viscous Flow Through Multistage Turbomachines," ASME J. Turbomach., 114, pp. 18-26.
-
(1992)
ASME J. Turbomach.
, vol.114
, pp. 18-26
-
-
Denton, J.D.1
-
16
-
-
0013384095
-
Axial flow compressor design
-
IMechE, HQ, London
-
Gallimore, S. J., 1998b, "Axial Flow Compressor Design," The Successful Exploitation of CFD in Turbomachinery Design, IMechE, HQ, London.
-
(1998)
The Successful Exploitation of CFD in Turbomachinery Design
-
-
Gallimore, S.J.1
-
17
-
-
0343232030
-
-
Rolls Royce plc, private communication, Compressor Design
-
Gallimore, S. J., 1999, Rolls Royce plc, private communication, Compressor Design.
-
(1999)
-
-
Gallimore, S.J.1
-
18
-
-
0003445026
-
-
ASME Paper No. 94-GT-151
-
Chen, J. P., Celestina, M. L., and Adamczyk, J. J., 1994, "A New Procedure for Simulating Unsteady Flows Through Turbomachinery Blade Passages," ASME Paper No. 94-GT-151.
-
(1994)
A New Procedure for Simulating Unsteady Flows Through Turbomachinery Blade Passages
-
-
Chen, J.P.1
Celestina, M.L.2
Adamczyk, J.J.3
-
19
-
-
0003747684
-
-
AIAA Paper No. 90-2354
-
Dorney, D. J., Davis, R. L., Edwards, D. E., and Madavan, N. K., 1990, "Unsteady Analysis of Hot Streak Migration in a Turbine Stage," AIAA Paper No. 90-2354.
-
(1990)
Unsteady Analysis of Hot Streak Migration in a Turbine Stage
-
-
Dorney, D.J.1
Davis, R.L.2
Edwards, D.E.3
Madavan, N.K.4
-
20
-
-
0025495158
-
Stator/rotor interactions in a transonic turbine
-
Giles, M. B., 1990, "Stator/Rotor Interactions in a Transonic Turbine," AIAA J. Propulsion Power, 6, p. 621.
-
(1990)
AIAA J. Propulsion Power
, vol.6
, pp. 621
-
-
Giles, M.B.1
-
21
-
-
0026143136
-
Temporally and spatially resolved flow in a two-stage axial compressor: Part 2 - Computational assessment
-
Gundy-Burlet, K. L., Rai, M. M., Stauter, R. C., and Dring, R. P., 1991, "Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 2 - Computational Assessment," ASME J. Turbomach., 113, No. 2, pp. 219-226.
-
(1991)
ASME J. Turbomach.
, vol.113
, Issue.2
, pp. 219-226
-
-
Gundy-Burlet, K.L.1
Rai, M.M.2
Stauter, R.C.3
Dring, R.P.4
-
22
-
-
11644294150
-
On the interpretation of measured profile losses in unsteady wake-turbine blade interaction studies
-
Hodson, H. P., and Dawes, W. N., 1998, "On the Interpretation of Measured Profile Losses in Unsteady Wake-Turbine Blade Interaction Studies," ASME J. Turbomach., 120, p. 276.
-
(1998)
ASME J. Turbomach.
, vol.120
, pp. 276
-
-
Hodson, H.P.1
Dawes, W.N.2
-
24
-
-
0026745406
-
Assessment of unsteady flows in turbines
-
Sharma, O. P., Pickett, G. F., and Ni, R. H., 1992, "Assessment of Unsteady Flows in Turbines," ASME J. Turbomach., 114, pp. 79-90.
-
(1992)
ASME J. Turbomach.
, vol.114
, pp. 79-90
-
-
Sharma, O.P.1
Pickett, G.F.2
Ni, R.H.3
-
27
-
-
0343603453
-
Development and application of a multistage Navier-Stokes flow solver: Part II - Application to a high-pressure compressor design
-
LeJambre, C. R., Zacharias, R. M., Biederman, B. P., Gleixner, A. J., and Yetka, C. J., 1998, "Development and Application of a Multistage Navier-Stokes Flow Solver: Part II - Application to a High-Pressure Compressor Design," ASME J. Turbomach., 120, p. 215.
-
(1998)
ASME J. Turbomach.
, vol.120
, pp. 215
-
-
LeJambre, C.R.1
Zacharias, R.M.2
Biederman, B.P.3
Gleixner, A.J.4
Yetka, C.J.5
-
28
-
-
0343667702
-
-
AlliedSignal Engines, private communication, Multistage Compressor Simulations
-
Mansour, M., 1999, AlliedSignal Engines, private communication, Multistage Compressor Simulations.
-
(1999)
-
-
Mansour, M.1
-
29
-
-
0342362553
-
-
Rolls-Royce Allison, private communication, Multistage Compressor Simulations
-
Wellborn, S. R., 1999, Rolls-Royce Allison, private communication, Multistage Compressor Simulations.
-
(1999)
-
-
Wellborn, S.R.1
-
30
-
-
0003896102
-
-
NASA TP 1337
-
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.
-
(1978)
Design and Overall Performance of Four Highly Loaded, High-speed Inlet Stages for an Advanced High-pressure Ratio Core Compressor
-
-
Reid, L.1
Moore, R.2
-
32
-
-
0022793763
-
A model for closing the inviscid form of the average-passage equation system
-
Adamczyk, J. J., Mulac, R. A., and Celestina, M. L., 1986, "A Model for Closing the Inviscid Form of the Average-Passage Equation System," ASME J. Turbomach., 108, p. 180.
-
(1986)
ASME J. Turbomach.
, vol.108
, pp. 180
-
-
Adamczyk, J.J.1
Mulac, R.A.2
Celestina, M.L.3
-
33
-
-
0342362551
-
-
ASME Paper No. 99-GT-077
-
Kirtley, K. R., Turner, M. G., and Saeidi, S., 1999, "An Average-Passage Closure Model for General Meshes," ASME Paper No. 99-GT-077.
-
(1999)
An Average-passage Closure Model for General Meshes
-
-
Kirtley, K.R.1
Turner, M.G.2
Saeidi, S.3
-
34
-
-
0004738792
-
Development and application of a multistage Navier-Stokes solver: Part 1 - Multistage modeling using body forces and deterministic stresses
-
Rhie, C. M., Gleixner, A. J., Spear, D. A., Fischberg, C. J., and Zacharias, R. M., 1998, "Development and Application of a Multistage Navier-Stokes Solver: Part 1 - Multistage Modeling Using Body Forces and Deterministic Stresses," ASME J. Turbomach., 120, p. 205.
-
(1998)
ASME J. Turbomach.
, vol.120
, pp. 205
-
-
Rhie, C.M.1
Gleixner, A.J.2
Spear, D.A.3
Fischberg, C.J.4
Zacharias, R.M.5
-
35
-
-
85024521745
-
A mathematical constraint placed upon inter-blade row boundary conditions used in the simulation of multistage turbomachinery flows
-
CFD Techniques for Propulsion Applications
-
Adamczyk, J. J., 1991, "A Mathematical Constraint Placed Upon Inter-Blade Row Boundary Conditions Used in The Simulation of Multistage Turbomachinery Flows," AGARD Conf. Proc. 510, CFD Techniques for Propulsion Applications.
-
(1991)
AGARD Conf. Proc.
, vol.510
-
-
Adamczyk, J.J.1
-
36
-
-
0019933509
-
Span-wise mixing in multistage axial flow compressors
-
Adkins, Jr, G. G., and Smith, Jr, L. H., 1982, "Span-wise Mixing in Multistage Axial Flow Compressors," ASME J. Eng. Power, , 104, p. 97.
-
(1982)
ASME J. Eng. Power,
, vol.104
, pp. 97
-
-
Adkins G.G., Jr.1
Smith L.H., Jr.2
-
37
-
-
84925865729
-
Spanwise transport in axial-flow turbines: Part 1 - The multistage environment
-
Lewis, K. L., 1993, "Spanwise Transport in Axial-Flow Turbines: Part 1 - The Multistage Environment," ASME J. Turbomach., 116, pp. 179-186.
-
(1993)
ASME J. Turbomach.
, vol.116
, pp. 179-186
-
-
Lewis, K.L.1
-
38
-
-
0027948764
-
Spanwise transport in axial-flow turbines: Part 2 - Throughflow calculations
-
Lewis, K. L., 1994, "Spanwise Transport in Axial-Flow Turbines: Part 2 - Throughflow Calculations," ASME J. Turbomach., 116, pp. 187-193.
-
(1994)
ASME J. Turbomach.
, vol.116
, pp. 187-193
-
-
Lewis, K.L.1
-
39
-
-
85002855885
-
Redistribution of an inlet temperature distortion in an axial flow turbine stage
-
Butler, T. L., Sharma, O. P., Joslyn, H. D., and Dring R. P., 1989, "Redistribution of an Inlet Temperature Distortion in an Axial Flow Turbine Stage," AIAA J. Propulsion Power, 5.
-
(1989)
AIAA J. Propulsion Power
, pp. 5
-
-
Butler, T.L.1
Sharma, O.P.2
Joslyn, H.D.3
Dring, R.P.4
-
41
-
-
85069385330
-
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, p. 359.
-
(1970)
ASME J. Eng. Power
, vol.92
, pp. 359
-
-
Kerrebrock, J.L.1
Mikolajczak, A.A.2
-
42
-
-
0343667693
-
-
SAE Paper No. 931375
-
Kirtley, K. R., Celestina, M. L., and Adamczyk, J. J., 1993, "The Effect of Unsteadiness on the Time-Mean Thermal Loads in a Turbine Stage," SAE Paper No. 931375.
-
(1993)
The Effect of Unsteadiness on the Time-mean Thermal Loads in a Turbine Stage
-
-
Kirtley, K.R.1
Celestina, M.L.2
Adamczyk, J.J.3
-
44
-
-
0027277266
-
Control of the unsteady flow in a stator blade row interacting with upstream moving wakes
-
Valkov, T., and Tan, C. S., 1993, "Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes," ASME J. Turbomach., 117, pp. 97-105.
-
(1993)
ASME J. Turbomach.
, vol.117
, pp. 97-105
-
-
Valkov, T.1
Tan, C.S.2
-
45
-
-
0032702071
-
Effect of upstream rotor vortical disturbances on the time-average performance of axial compressor stators: Part 1 - Framework of technical approach and wake-stator blade interactions
-
Valkov, T. V., and Tan, C. S., 1998, "Effect of Upstream Rotor Vortical Disturbances on the Time-Average Performance of Axial Compressor Stators: Part 1 - Framework of Technical Approach and Wake-Stator Blade Interactions," ASME J. Turbomach., 121, pp. 377-386.
-
(1998)
ASME J. Turbomach.
, vol.121
, pp. 377-386
-
-
Valkov, T.V.1
Tan, C.S.2
-
46
-
-
0032723963
-
Effect of upstream rotor vortical disturbances on the time-average performance of axial compressor stators: Part 2 - Rotor tip vortex/streamwise vortex-stator blade interactions
-
Valkov, T. V., and Tan, C. S., 1999, "Effect of Upstream Rotor Vortical Disturbances on the Time-Average Performance of Axial Compressor Stators: Part 2 - Rotor Tip Vortex/Streamwise Vortex-Stator Blade Interactions," ASME J. Turbomach., 121, pp. 386-396.
-
(1999)
ASME J. Turbomach.
, vol.121
, pp. 386-396
-
-
Valkov, T.V.1
Tan, C.S.2
-
48
-
-
84925935463
-
An asymptotic analysis of mixing loss
-
Fritsch, G., and Giles, M. B., 1993, "An Asymptotic Analysis of Mixing Loss," ASME J. Turbomach., 117, pp. 367-374.
-
(1993)
ASME J. Turbomach.
, vol.117
, pp. 367-374
-
-
Fritsch, G.1
Giles, M.B.2
-
49
-
-
84973651742
-
Wake dispersion in turbomachines
-
Smith, Jr, L. H., 1996, "Wake Dispersion in Turbomachines," ASME J. Basic Eng., 88, No. 3.
-
(1996)
ASME J. Basic Eng.
, vol.88
, Issue.3
-
-
Smith L.H., Jr.1
-
53
-
-
0004086913
-
-
ASME Paper No. 97-GT-535
-
Van Zante, D. E., Adamczyk, J. J., Strazisar, A. J., and Okiishi, T. H., 1997, "Wake Recovery Performance Benefit in a High-Speed Axial Flow Compressor," ASME Paper No. 97-GT-535.
-
(1997)
Wake Recovery Performance Benefit in a High-speed Axial Flow Compressor
-
-
Van Zante, D.E.1
Adamczyk, J.J.2
Strazisar, A.J.3
Okiishi, T.H.4
-
55
-
-
0342797367
-
-
Discussion of ASME Paper No. 96-GT-029 and ASME Paper No. 96-GT-253, Birmingham, United Kingdom
-
Smith, L. H., Jr., 1996, Discussion of ASME Paper No. 96-GT-029 and ASME Paper No. 96-GT-253, Birmingham, United Kingdom.
-
(1996)
-
-
Smith L.H., Jr.1
-
57
-
-
0027224136
-
Blade row interaction in a multistage low-pressure turbine
-
Arndt, N., 1993, "Blade Row Interaction in a Multistage Low-Pressure Turbine," ASME J. Turbomach., 115, pp. 137-146.
-
(1993)
ASME J. Turbomach.
, vol.115
, pp. 137-146
-
-
Arndt, N.1
-
58
-
-
0342362536
-
Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
-
Sharma, O. P., Stetson, G. M., Daniels, W. A., Greitzer, E. D., Blair, M. F., and Dring, R. P., 1997, "Impact of Periodic Unsteadiness on Performance and Heat Load in Axial Flow Turbomachines," NASA Contractor Report No. 202319.
-
(1997)
NASA Contractor Report No. 202319
-
-
Sharma, O.P.1
Stetson, G.M.2
Daniels, W.A.3
Greitzer, E.D.4
Blair, M.F.5
Dring, R.P.6
-
60
-
-
84961307305
-
Numerical simulation of multi-stage turbomachinery flows
-
Toulouse, France, May 11-15
-
Adamczyk, J. J., Hathaway, M. D., Shabbir, A., and Wellborn, S. R., 1998, "Numerical Simulation of Multi-Stage Turbomachinery Flows," presented at the Applied Vehicle Technology Symposium on Design Principles and Methods for Aircraft Gas Turbine Engines, Toulouse, France, May 11-15.
-
(1998)
Applied Vehicle Technology Symposium on Design Principles and Methods for Aircraft Gas Turbine Engines
-
-
Adamczyk, J.J.1
Hathaway, M.D.2
Shabbir, A.3
Wellborn, S.R.4
-
61
-
-
0343667682
-
-
NASA CR-168245
-
Cline, S. J., Fesler, W., Liu, H. T., Lovell, R. C., and Shaffer, S. J., 1977, "Energy Efficient Engine, High Pressure Compressor Component Performance Report," NASA CR-168245.
-
(1977)
Energy Efficient Engine, High Pressure Compressor Component Performance Report
-
-
Cline, S.J.1
Fesler, W.2
Liu, H.T.3
Lovell, R.C.4
Shaffer, S.J.5
-
62
-
-
0342362523
-
-
NASA CR 135133
-
Wisler, D. C., Koch, C. C., Smith, L. H., Jr., 1977, "Energy Efficient Engine, Preliminary Design Study of Advanced Multistage Axial Flow Core Compressors," NASA CR 135133.
-
(1977)
Energy Efficient Engine, Preliminary Design Study of Advanced Multistage Axial Flow Core Compressors
-
-
Wisler, D.C.1
Koch, C.C.2
Smith L.H., Jr.3
-
63
-
-
0343667672
-
-
GE Aircraft Engines, private communication, CAF-MIX II Development
-
Smith, L. H., Jr., 1999, GE Aircraft Engines, private communication, CAF-MIX II Development.
-
(1999)
-
-
Smith L.H., Jr.1
-
64
-
-
0342797400
-
-
private communication, Blockage Estimates
-
Turner, M. G., 1999, private communication, Blockage Estimates.
-
(1999)
-
-
Turner, M.G.1
-
65
-
-
0343231992
-
-
GE Aircraft Engines, private communication. Compressor Stall
-
Liu, H. T., 1999, GE Aircraft Engines, private communication. Compressor Stall.
-
(1999)
-
-
Liu, H.T.1
-
66
-
-
0031340590
-
-
ASME Paper No. 97-GT-346
-
Shabbir, A., Celestina, M. L., Adamczyk, J. J., and Strazisar, A. J., 1997, "The Effect of Hub Leakage Flow on Two High Speed Axial Flow Compressor Rotors," ASME Paper No. 97-GT-346.
-
(1997)
The Effect of Hub Leakage Flow on Two High Speed Axial Flow Compressor Rotors
-
-
Shabbir, A.1
Celestina, M.L.2
Adamczyk, J.J.3
Strazisar, A.J.4
-
68
-
-
84971500531
-
The influence of shrouded stator cavity flows on multistage compressor performance
-
Wellborn, S. R., and Okiishi, T. H., 1998, "The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance," ASME J. Turbomach., 121, pp. 486-497.
-
(1998)
ASME J. Turbomach.
, vol.121
, pp. 486-497
-
-
Wellborn, S.R.1
Okiishi, T.H.2
-
69
-
-
0027627493
-
Blade row interaction effects on compressor measurements
-
Shang, T., Epstein, A. H., Giles, M. B., and Sehra, A., 1993, "Blade Row Interaction Effects on Compressor Measurements," AIAA J. Propulsion Power, 9, No. 4, p. 569.
-
(1993)
AIAA J. Propulsion Power
, vol.9
, Issue.4
, pp. 569
-
-
Shang, T.1
Epstein, A.H.2
Giles, M.B.3
Sehra, A.4
-
71
-
-
0343667673
-
-
ASME Paper No. 95-GT-443
-
Cumpsty, N. A., Dong, Y., and Li, Y. S., 1995, "Compressor Blade Boundary Layers in the Presence of Wakes," ASME Paper No. 95-GT-443.
-
(1995)
Compressor Blade Boundary Layers in the Presence of Wakes
-
-
Cumpsty, N.A.1
Dong, Y.2
Li, Y.S.3
-
72
-
-
0030935568
-
Boundary layer development in axial compressors and turbines: Part I of 4 - Composite picture
-
Halstead, D. E., Wisler, D. C., Okiishi, T. H., Walker, G. J., Hodson, H. P., and Shin, H., 1997, "Boundary Layer Development in Axial Compressors and Turbines: Part I of 4 - Composite Picture," ASME J. Turbomach., 119, p. 114.
-
(1997)
ASME J. Turbomach.
, vol.119
, pp. 114
-
-
Halstead, D.E.1
Wisler, D.C.2
Okiishi, T.H.3
Walker, G.J.4
Hodson, H.P.5
Shin, H.6
-
73
-
-
85007924016
-
Modeling unsteady transition and its effects on profile loss
-
Hodson, H. P., 1990, "Modeling Unsteady Transition and Its Effects on Profile Loss," ASME J. Turbomach., 112, pp. 691-701.
-
(1990)
ASME J. Turbomach.
, vol.112
, pp. 691-701
-
-
Hodson, H.P.1
-
75
-
-
0001940985
-
The role of research in the aerodynamic design of an advanced low pressure turbine
-
IMechE, London, Mar.
-
Harvey, N. W., Schulte, V. S., Howell, R. J., and Hodson, H. P., 1999, "The Role of Research in the Aerodynamic Design of an Advanced Low Pressure Turbine," Proc. 3rd European Conf. on Turbomachinery, IMechE, London, Mar.
-
(1999)
Proc. 3rd European Conf. on Turbomachinery
-
-
Harvey, N.W.1
Schulte, V.S.2
Howell, R.J.3
Hodson, H.P.4
-
76
-
-
0016034522
-
The numerical computation of turbulent flows
-
Launder, B. E., and Spalding, D. B., 1974, "The Numerical Computation of Turbulent Flows," Comp. Math. Appl. Mech., 3, p. 269.
-
(1974)
Comp. Math. Appl. Mech.
, vol.3
, pp. 269
-
-
Launder, B.E.1
Spalding, D.B.2
-
77
-
-
0029277647
-
A new k - ∈ Eddy viscosity model for high reynolds number turbulent flows
-
Shih, T. H., Liou, W. W., Shabbir, A., Zhu, J., and Yang, Z., 1995, "A New k - ∈ Eddy Viscosity Model for High Reynolds Number Turbulent Flows," Comp. Fluids, 23, No. 3, p. 227.
-
(1995)
Comp. Fluids
, vol.23
, Issue.3
, pp. 227
-
-
Shih, T.H.1
Liou, W.W.2
Shabbir, A.3
Zhu, J.4
Yang, Z.5
-
78
-
-
0022812702
-
Rotor wake characteristics of a transonic axial-flow fan
-
Hathaway, M. D., Gertz, J. B., Epstein, A. H., and Strazisar, A. J., 1986, "Rotor Wake Characteristics of a Transonic Axial-Flow Fan," AIAA J., 24, No. 11, p. 1802.
-
(1986)
AIAA J.
, vol.24
, Issue.11
, pp. 1802
-
-
Hathaway, M.D.1
Gertz, J.B.2
Epstein, A.H.3
Strazisar, A.J.4
-
79
-
-
0026143138
-
Unsteady radial transport in a transonic compressor stage
-
Kotidis, P. A., and Epstein, A. H., 1991, "Unsteady Radial Transport in a Transonic Compressor Stage," ASME J. Turbomach., 113, pp. 207-218.
-
(1991)
ASME J. Turbomach.
, vol.113
, pp. 207-218
-
-
Kotidis, P.A.1
Epstein, A.H.2
-
80
-
-
0022043947
-
An experimental investigation into the effect of wakes on the unsteady turbine rotor flow
-
Binder, A., Foster, W., Kruse, H., and Rogge, H., 1985, "An Experimental Investigation Into the Effect of Wakes on the Unsteady Turbine Rotor Flow," ASME J. Eng. Mater. Technol., 107, p. 458.
-
(1985)
ASME J. Eng. Mater. Technol.
, vol.107
, pp. 458
-
-
Binder, A.1
Foster, W.2
Kruse, H.3
Rogge, H.4
-
81
-
-
0342362499
-
-
ASME Paper No. 95-GT-240
-
van de Wall, A. G., Kadambi, J. R., Boyle, R. J., and Adamczyk, J. J., 1995, "The Transport of Vorticies Through a Turbine Cascade," ASME Paper No. 95-GT-240.
-
(1995)
The Transport of Vorticies Through a Turbine Cascade
-
-
Van De Wall, A.G.1
Kadambi, J.R.2
Boyle, R.J.3
Adamczyk, J.J.4
-
82
-
-
0040779788
-
-
Applied Research Lab. Penn. State Univ. T. R.
-
Zierke, W. C., Straka, W. A., and Taylor, T. D., 1993, "The High Reynolds Number Flow Through an Axial Flow Pump," Applied Research Lab. Penn. State Univ. T. R. 93-12.
-
(1993)
The High Reynolds Number Flow Through an Axial Flow Pump
, pp. 93-112
-
-
Zierke, W.C.1
Straka, W.A.2
Taylor, T.D.3
-
83
-
-
0013376047
-
-
ASME Paper No. 99-GT-99
-
Graf, M. B., Greitzer, E. M., Marble, F. E., and Sharma, O. P., 1999, "Effects of Stator Pressure Field on Upstream Rotor Performance," ASME Paper No. 99-GT-99.
-
(1999)
Effects of Stator Pressure Field on Upstream Rotor Performance
-
-
Graf, M.B.1
Greitzer, E.M.2
Marble, F.E.3
Sharma, O.P.4
|