메뉴 건너뛰기




Volumn , Issue , 1996, Pages

Performance prediction of endwall treated fan rotors with inflow distortion

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING;

EID: 85086949789     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-244     Document Type: Conference Paper
Times cited : (6)

References (40)
  • 2
    • 10244238227 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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
  • 7
    • 0021468795 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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
  • 15
    • 0027626743 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고    scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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
  • 28
    • 0007625295 scopus 로고
    • 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 scopus 로고
    • 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
  • 31
    • 85001943704 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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
  • 35
    • 84926058564 scopus 로고
    • 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
  • 39
    • 0007625295 scopus 로고
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.