-
1
-
-
4243643880
-
-
NASA TN D-6538
-
Moore, R. D., Kovich, G., and Blade, R. J., "Effect of Casing Treatment on Overall and Blade-Element Performance of a Compressor Rotor," NASA TN D-6538. 1971.
-
(1971)
Effect of Casing Treatment on Overall and Blade-Element Performance of a Compressor Rotor
-
-
Moore, R.D.1
Kovich, G.2
Blade, R.J.3
-
2
-
-
10244238227
-
Effect of Several Porous Casing Treatments on Stall Limit and on Overall Performance of an Axial Compressor Rotor
-
Osborn, W. M., Lewis, G. W., and Heidelberg, L. J., "Effect of Several Porous Casing Treatments on Stall Limit and on Overall Performance of an Axial Compressor Rotor," NASA TN D-6537, 1971.
-
(1971)
NASA TN D-6537
-
-
Osborn, W.M.1
Lewis, G.W.2
Heidelberg, L.J.3
-
3
-
-
10244250838
-
Study of Casing Treatment Stall Margin Improvement Phenomena
-
Prince, D. C., Jr., Wisler, D. C., and Hilvers, D. E., "Study of Casing Treatment Stall Margin Improvement Phenomena," NASA CR-134552, 1974.
-
(1974)
NASA CR-134552
-
-
Prince, D.C.1
Wisler, D.C.2
Hilvers, D.E.3
-
4
-
-
0021475580
-
A Study of Configurations of Casing Treatment for Axial Flow Compressors
-
of JSME, Vol. 27, No. 230, 1985, pp. 1675-1681
-
Fujita, H., and Takata, H., "A Study of Configurations of Casing Treatment for Axial Flow Compressors," Bull, of JSME, Vol. 27, No. 230, 1985, pp. 1675-1681.
-
Bull
-
-
Fujita, H.1
Takata, H.2
-
5
-
-
0017427966
-
Stall Margin Improvement by Casing Treatment-Its Mechanism and Effectiveness
-
Takata, H., and Tsukuda, Y., "Stall Margin Improvement by Casing Treatment-Its Mechanism and Effectiveness," ASME Journal of Engineering for Power, Vol. 99, 1977, pp.121-133.
-
(1977)
ASME Journal of Engineering for Power
, vol.99
, pp. 121-133
-
-
Takata, H.1
Tsukuda, Y.2
-
6
-
-
0021459635
-
Flow Phenomena in Compressor Casing Treatment
-
Smith, G. D. J., and Cumpsty, N. A., "Flow Phenomena in Compressor Casing Treatment," ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, 1985, pp. 532-541.
-
(1985)
ASME Journal of Engineering for Gas Turbines and Power
, vol.107
, pp. 532-541
-
-
Smith, G.D.J.1
Cumpsty, N.A.2
-
7
-
-
0021468795
-
Effects of Compressor Hub Treatment on Stator Stall Margin and Performance
-
Cheng, P., Prell, M. E., Greitzer, E. M., and Tan, C. S., "Effects of Compressor Hub Treatment on Stator Stall Margin and Performance," Journal of Aircraft, Vol. 21, No. 7, 1984, pp. 469-475.
-
(1984)
Journal of Aircraft
, vol.21
, Issue.7
, pp. 469-475
-
-
Cheng, P.1
Prell, M.E.2
Greitzer, E.M.3
Tan, C.S.4
-
8
-
-
0023383225
-
Effects of Slotted Hub and Casing Treatments on Compressor End wall Flow Fields
-
Johnson, M. C., and Greitzer, E. M., "Effects of Slotted Hub and Casing Treatments on Compressor End wall Flow Fields," ASME Journal of Turbomachinery, Vol. 109, 1987, pp. 380-387.
-
(1987)
ASME Journal of Turbomachinery
, vol.109
, pp. 380-387
-
-
Johnson, M.C.1
Greitzer, E.M.2
-
9
-
-
0025249452
-
Effects of Endwall Suction and Blowing on Compressor Stability Enhancement
-
Lee, N. K. W., and Greitzer, E. M., "Effects of Endwall Suction and Blowing on Compressor Stability Enhancement," ASME Journal of Turbomachinery, Vol. 112, 1990, pp. 133-144.
-
(1990)
ASME Journal of Turbomachinery
, vol.112
, pp. 133-144
-
-
Lee, N.K.W.1
Greitzer, E.M.2
-
11
-
-
0022108323
-
The Performance Characteristic of an Air-separator of an Axial Flow Fan
-
of JSME, Vol. 28, No. 242, 1985, pp. 1659-1666
-
Miyake, Y., Noji, I., Nishikawa, Y., and Murata, S., "The Performance Characteristic of an Air-separator of an Axial Flow Fan," Bull, of JSME, Vol. 28, No. 242, 1985, pp. 1659-1666.
-
Bull
-
-
Miyake, Y.1
Noji, I.2
Nishikawa, Y.3
Murata, S.4
-
12
-
-
85011573109
-
A Tip Treatment for Axial Flow Fans and Compressors
-
April
-
Azimian, A. R., McKenzie, A. B., and Elder, R. L., "A Tip Treatment for Axial Flow Fans and Compressors," IMechE, April 1987.
-
(1987)
IMechE
-
-
Azimian, A.R.1
McKenzie, A.B.2
Elder, R.L.3
-
13
-
-
34548781698
-
-
ASME 89-GT-68
-
Azimian, A. R., Elder, R. L., and McKenzie, A. B., "Application of Recess Vaned Casing Treatment to Axial Flow Fans," ASME 89-GT-68.
-
Application of Recess Vaned Casing Treatment to Axial Flow Fans
-
-
Azimian, A.R.1
Elder, R.L.2
McKenzie, A.B.3
-
14
-
-
0018300976
-
A Fundamental Criterion for the Application of Rotor Casing Treatment
-
June
-
Greitzer, E. M., Nikkanen, J. P., Haddad, D. E., Mazzaway, R. S., Joslyn, H. D., "A Fundamental Criterion for the Application of Rotor Casing Treatment," Journal of Fluids Engineering, Vol. 101, June, 1979, pp. 237-242.
-
(1979)
Journal of Fluids Engineering
, vol.101
, pp. 237-242
-
-
Greitzer, E.M.1
Nikkanen, J.P.2
Haddad, D.E.3
Mazzaway, R.S.4
Joslyn, H.D.5
-
15
-
-
0027626743
-
Numerical Simulation of Compressor Endwall and Casing Treatment Flow Phenomena
-
Crook, A. J., Greitzer, E. M., Tan, C. S., and Adamczyk, J. J., "Numerical Simulation of Compressor Endwall and Casing Treatment Flow Phenomena," ASME Journal of Turbomachinery, Vol. 115, No. 3, pp. 501-512.
-
ASME Journal of Turbomachinery
, vol.115
, Issue.3
, pp. 501-512
-
-
Crook, A.J.1
Greitzer, E.M.2
Tan, C.S.3
Adamczyk, J.J.4
-
17
-
-
0003284193
-
A Survey of Inlet Engine Distortion Capability
-
prepared for AIAA Joint Propulsion Specialists Conference, June
-
Bowditch, D.N., Coltrin, R.E., "A Survey of Inlet Engine Distortion Capability," NASA TM-83421, prepared for AIAA Joint Propulsion Specialists Conference, June 1983.
-
(1983)
NASA TM-83421
-
-
Bowditch, D.N.1
Coltrin, R.E.2
-
18
-
-
0003400572
-
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
-
May
-
SAE Aerospace Council Division Technical Committee S-l6, "Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines," SAE Aerospace Information Report AIR-1419, May 1983.
-
(1983)
SAE Aerospace Information Report AIR-1419
-
-
-
19
-
-
84997181835
-
Multiple Segment Parallel Compressor Model for Circumfer-ential Flow Distortion
-
April 1977, pp. 288296
-
Mazzawy, R.S., "Multiple Segment Parallel Compressor Model for Circumfer-ential Flow Distortion," ASME Journal of En-gneering for Power, April 1977, pp. 288296.
-
ASME Journal of En-gneering for Power
-
-
Mazzawy, R.S.1
-
20
-
-
0023384319
-
A Method for Assessing Effects of Circumferential Flow Distortion on Compressor Stability
-
July
-
Hynes, T.P. and Greitzer, E.M., "A Method for Assessing Effects of Circumferential Flow Distortion on Compressor Stability," ASME Journal of Turbomachinery, Vol. 109, July 1987, pp. 371-379.
-
(1987)
ASME Journal of Turbomachinery
, vol.109
, pp. 371-379
-
-
Hynes, T.P.1
Greitzer, E.M.2
-
21
-
-
19244368019
-
Calculations of Inlet Distortion-Induced Compressor Flow Field Instability
-
Chue, R., et al., "Calculations of Inlet Distortion-Induced Compressor Flow Field Instability" International Journal of Heat and Fluid Flow, Vol. 10, 1989, pp. 211-223.
-
(1989)
International Journal of Heat and Fluid Flow
, vol.10
, pp. 211-223
-
-
Chue, R.1
-
22
-
-
0011458949
-
Aerodynamic Analysis of Compressor Casing Treatment with a 3-D Navier-Stokes Solver
-
Hall, Edward J., Crook, Andrew J., and Delaney, Robert A., "Aerodynamic Analysis of Compressor Casing Treatment with a 3-D Navier-Stokes Solver," AIAA Paper 94-2796, 1994.
-
(1994)
AIAA Paper 94-2796
-
-
Hall, E.J.1
Crook, A.J.2
Delaney, R.A.3
-
23
-
-
10244220353
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task I-Ducted Propfan Analysis
-
NASA Contract NAS3-25270
-
Hall, E. J., Delaney, R. A., and Bettner, J. L., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task I-Ducted Propfan Analysis," NASA CR 185217, NASA Contract NAS3-25270, 1990.
-
(1990)
NASA CR 185217
-
-
Hall, E.J.1
Delaney, R.A.2
Bettner, J.L.3
-
24
-
-
10244225715
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task II-Unsteady Ducted Propfan Analysis-Final Report
-
NASA Contract NAS3-25270
-
Hall, E. J. and Delaney, R. A., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task II-Unsteady Ducted Propfan Analysis-Final Report," NASA CR 187106, NASA Contract NAS3-25270, 1992.
-
(1992)
NASA CR 187106
-
-
Hall, E.J.1
Delaney, R.A.2
-
25
-
-
10244225715
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task V-Counterrotation Ducted Propfan Analysis, Final Report
-
NASA Contract NAS3-25270
-
Hall, E. J. and Delaney, R. A., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task V-Counterrotation Ducted Propfan Analysis, Final Report," NASA CR 187126, NASA Contract NAS3-25270, 1992.
-
(1992)
NASA CR 187126
-
-
Hall, E.J.1
Delaney, R.A.2
-
26
-
-
10244278471
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VIII-Cooling Flow/Heat Transfer Analysis, Final Report
-
September
-
Hall, E. J., Topp, D. A., Heidegger, N. J., and Delaney, R. A., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VIII-Cooling Flow/Heat Transfer Analysis, Final Report," NASA CR 195359, September, 1994.
-
(1994)
NASA CR 195359
-
-
Hall, E.J.1
Topp, D.A.2
Heidegger, N.J.3
Delaney, R.A.4
-
27
-
-
84997638205
-
Preliminary Findings in Certification of ADPAC
-
June
-
Barber, T., Choi, D., McNulty, G., Hall, E., and Delaney, R., " Preliminary Findings in Certification of ADPAC," AIAA Paper 94-2240, June, 1994.
-
(1994)
AIAA Paper 94-2240
-
-
Barber, T.1
Choi, D.2
McNulty, G.3
Hall, E.4
Delaney, R.5
-
28
-
-
0007625295
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VII-ADPAC User's Manual
-
NASA CR 195472, July
-
Hall, E. J., and Delaney, R. A., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VII-ADPAC User's Manual," NASA Contract NAS3-25270, NASA CR 195472, July, 1995.
-
(1995)
NASA Contract NAS3-25270
-
-
Hall, E.J.1
Delaney, R.A.2
-
29
-
-
0001097696
-
Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes
-
Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes," AIAA Paper 81-1259, 1981.
-
(1981)
AIAA Paper 81-1259
-
-
Jameson, A.1
Schmidt, W.2
Turkel, E.3
-
30
-
-
0024858972
-
Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
-
Adamczyk, J. J., Celestina, M. L., Beach, T. A., and Barnett, M., "Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine," ASME Paper 89-GT-152, 1989.
-
(1989)
ASME Paper 89-GT-152
-
-
Adamczyk, J.J.1
Celestina, M.L.2
Beach, T.A.3
Barnett, M.4
-
31
-
-
85001943704
-
An Unconditionally Stable Runge-Kutta Method for Unsteady Flows
-
Jorgensen, P. C. E., and Chima, R. V., "An Unconditionally Stable Runge-Kutta Method for Unsteady Flows," NASA TM 101347, 1989.
-
(1989)
NASA TM 101347
-
-
Jorgensen, P.C.E.1
Chima, R.V.2
-
32
-
-
0000104174
-
Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows
-
Baldwin, B. S., and Lomax, H.M. "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, 1978.
-
(1978)
AIAA Paper 78-257
-
-
Baldwin, B.S.1
Lomax, H.M.2
-
33
-
-
84962138089
-
Portable Programming on Parallel/Networked Computers Using the Application Portable Parallel Library (APPL)
-
Quealy, A., Cole, G. L., and Blech, R. A., "Portable Programming on Parallel/Networked Computers Using the Application Portable Parallel Library (APPL)," NASA TM-106238, 1993.
-
(1993)
NASA TM-106238
-
-
Quealy, A.1
Cole, G.L.2
Blech, R.A.3
-
34
-
-
0003798597
-
-
Oak Ridge National Lab Report ORNL/TM-12187, 1994
-
Geist, A., Beguelin, A., Dongarra, J., Jiang, W., Manchek, R., and Sunderam, V., "PVM 3 User's Guide and Reference Manual," Oak Ridge National Lab Report ORNL/TM-12187, 1994.
-
PVM 3 User's Guide and Reference Manual
-
-
Geist, A.1
Beguelin, A.2
Dongarra, J.3
Jiang, W.4
Manchek, R.5
Sunderam, V.6
-
35
-
-
84926058564
-
A Comparison of the Measured and Predicted Flowfield in a Modern Fan-Bypass Configuration
-
Goyal, R. K., and Dawes, W. N.,"A Comparison of the Measured and Predicted Flowfield in a Modern Fan-Bypass Configuration," ASME Paper 92-GT-298, 1992.
-
(1992)
ASME Paper 92-GT-298
-
-
Goyal, R.K.1
Dawes, W.N.2
-
37
-
-
84924794753
-
The Role of Tip Clearance in High-Speed Fan Stall
-
Adamczyk, J. J., Celestina, M. L., and Greitzer, E. M., "The Role of Tip Clearance in High-Speed Fan Stall" ASME Paper 91-GT-83, 1991.
-
(1991)
ASME Paper 91-GT-83
-
-
Adamczyk, J.J.1
Celestina, M.L.2
Greitzer, E.M.3
-
39
-
-
0007625295
-
Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VII-Endwall Treatment Inlet Flow Distortion Analysis Final Report
-
NASA CR-195468, July
-
Hall, E. J., Topp, D, A., Heidegger, N. J., and Delaney, R. A., "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VII-Endwall Treatment Inlet Flow Distortion Analysis Final Report," NASA Contract NAS3-25270, NASA CR-195468, July, 1995.
-
(1995)
NASA Contract NAS3-25270
-
-
Hall, E.J.1
Topp, D.A.2
Heidegger, N.J.3
Delaney, R.A.4
-
40
-
-
84999054844
-
Multigrid Time-Accurate Integration of Navier-Stokes Equations
-
Arnone, A. A., Liou, M. S., and Povinelli, L. A., "Multigrid Time-Accurate Integration of Navier-Stokes Equations," AIAA Paper 93-3361-CP, 1993
-
(1993)
AIAA Paper 93-3361-CP
-
-
Arnone, A.A.1
Liou, M.S.2
Povinelli, L.A.3
|