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1
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0032194381
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Experiments in active control of stall on an aeroengine gas turbine
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Freeman, C., Wilson, A., Day, I.J., Swinbanks, M.A., 1998: Experiments in Active Control of Stall on an Aeroengine Gas Turbine, ASME Journal of Turbomachinery, 120, pp. 637-647.
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(1998)
ASME Journal of Turbomachinery
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Freeman, C.1
Wilson, A.2
Day, I.J.3
Swinbanks, M.A.4
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2
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0034233216
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Active stabilization of surge in an axi-centrifugal turboshaft engine
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Nelson, E.B., Paduano, J.D., Epstein, A.H., 2000: Active Stabilization of Surge in an Axi-Centrifugal Turboshaft Engine, ASME Journal of Turbomachinery, 122, pp. 485-493.
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(2000)
ASME Journal of Turbomachinery
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Nelson, E.B.1
Paduano, J.D.2
Epstein, A.H.3
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3
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0032703439
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Rotating stall control in a high-speed stage with inlet distortion, part I-radial distortion
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Spakovszky, Z.S., Weigl, H.J., Paduano, J.D., van Schalkwyk, C.M., Suder, K.L., Bright, M.M., 1999: Rotating Stall Control in a High-Speed Stage with Inlet Distortion, Part I-Radial Distortion, ASME J. of Turbomachinery, 121, Part I: pp. 510-516
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(1999)
ASME J. of Turbomachinery
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Spakovszky, Z.S.1
Weigl, H.J.2
Paduano, J.D.3
Van Schalkwyk, C.M.4
Suder, K.L.5
Bright, M.M.6
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4
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84885316780
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Part II-circumferential distortion
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Spakovsky, Z.S., Weigl, H.J., Paduano, J.D., van Schalkwyk, C. M., Suder, K.L., Bright, M.M., Part II-Circumferential Distortion, ibid., pp. 517-524.
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ASME J. of Turbomachinery
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Spakovsky, Z.S.1
Weigl, H.J.2
Paduano, J.D.3
Van Schalkwyk, C.M.4
Suder, K.L.5
Bright, M.M.6
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5
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0032194592
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Active stabilization of rotating stall in a transonic single stage axial compressor
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Weigl, H.J., Paduano, J.D., Fréchette, A.G., Epstein, A.H., Greitzer, E.M., Bright, M.M., Strazisar, A.J., 1998: Active Stabilization of Rotating Stall in a Transonic Single Stage Axial Compressor, ASME J. of Turbomachinery, 120, pp. 625-636.
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(1998)
ASME J. of Turbomachinery
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Weigl, H.J.1
Paduano, J.D.2
Fréchette, A.G.3
Epstein, A.H.4
Greitzer, E.M.5
Bright, M.M.6
Strazisar, A.J.7
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6
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0032979079
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Stall inception and the prospects for active control in four high speed compressors
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Day, I.J., Breuer, T., Escuret, J., Cherrett, W., Wilson, A., 1999: Stall Inception and the Prospects for Active Control in Four High Speed Compressors, ASME J. of Turbomachinery, 121, pp. 18-27.
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(1999)
ASME J. of Turbomachinery
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Day, I.J.1
Breuer, T.2
Escuret, J.3
Cherrett, W.4
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7
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0342700197
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Stall inception in the compressor system of a turbofan engine
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Höss, B., Leinhos, D.C., Fottner, L., 2000: Stall Inception in the Compressor System of a Turbofan Engine, ASME J. of Turbomachinery, 122, pp. 32-44.
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(2000)
ASME J. of Turbomachinery
, vol.122
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Höss, B.1
Leinhos, D.C.2
Fottner, L.3
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8
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Active instability control of combustion oscillations in heavy duty gas turbines
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Hermann, J., Orthmann, A., Hoffmann, S., 1999: Active Instability Control of Combustion Oscillations in Heavy Duty Gas Turbines, 6th International Congress on Sound and Vibration, Copenhagen, Denmark.
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(1999)
6th International Congress on Sound and Vibration, Copenhagen, Denmark
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Hermann, J.1
Orthmann, A.2
Hoffmann, S.3
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9
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85087603356
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Active stabilization of a low pressure compressor in a turbofan engine with constant air injection
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AIAA-2001-3312
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Leinhos, D.C., Scheidler, S., Fottner, L., 2001: Active Stabilization of a Low Pressure Compressor in a Turbofan Engine with Constant Air Injection, 37th AIAA/ASME/SAE/ASEE Joint Prop. Conf., Salt Lake City, USA, July 8-11, AIAA-2001-3312.
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(2001)
37th AIAA/ASME/SAE/ASEE Joint Prop. Conf., Salt Lake City, USA, July 8-11
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Leinhos, D.C.1
Scheidler, S.2
Fottner, L.3
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10
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33645785108
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A system for monitoring, measurement and analysis of transient performance and stall phenomena of gas turbine engines
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IEEE Publication 93CH3199-7
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Herpel, Th., Fottner, L., 1993: A System for Monitoring, Measurement and Analysis of Transient Performance and Stall Phenomena of Gas Turbine Engines, ICIASF '93 Record, IEEE Publication 93CH3199-7.
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ICIASF '93 Record
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Herpel, Th.1
Fottner, L.2
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11
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84885305442
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Aufbau und Untersuchung einer Pumpgrenzregelung am Turbostrahltriebwerk Larzac 04, Diplomarbeit 2001/5.3
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Institut für Strahlantriebe, Universität der Bundeswehr München, Germany
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Petitjean, A., 2001: Aufbau und Untersuchung einer Pumpgrenzregelung am Turbostrahltriebwerk Larzac 04, Diplomarbeit 2001/5.3, Institut für Strahlantriebe, Universität der Bundeswehr München, Germany.
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(2001)
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Petitjean, A.1
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12
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0034877484
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The influence of transient inlet distortions on the instability inception of a low pressure compressor in a turbofan engine
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Leinhos, D.C., Schmid, N.R., Fottner, L., 2001: The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine, ASME J. of Turbomachinery, 123, pp. 1-8.
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ASME J. of Turbomachinery
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Leinhos, D.C.1
Schmid, N.R.2
Fottner, L.3
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13
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4243397744
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Stall inception and surge in high-speed axial flow compressors
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AGARD CP-571 26/1-17
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Breuer, Th., Servaty, S. 1996: Stall Inception and Surge in High-Speed Axial Flow Compressors, AGARD CP-571 26/1-17.
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Breuer, Th.1
Servaty, S.2
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14
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0026143130
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Rotating waves as a stall inception indication in axial compressors
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Garnier, V.H., Epstein, A.H., Greitzer, E.M., 1992: Rotating Waves as a Stall Inception Indication in Axial Compressors, ASME Journal of Turbomachinery, 113, pp. 290-301.
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(1992)
ASME Journal of Turbomachinery
, vol.113
, pp. 290-301
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Garnier, V.H.1
Epstein, A.H.2
Greitzer, E.M.3
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15
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0029105769
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Pre-stall behavior of several high-speed compressors
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Tryfonidis, M., Etchevers, O., Paduano, J.D., Epstein, A.H., Hendricks, G.J., 1995: Pre-Stall Behavior of Several High-Speed Compressors, ASME Journal of Turbomachinery, 117, pp. 62-80.
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(1995)
ASME Journal of Turbomachinery
, vol.117
, pp. 62-80
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Tryfonidis, M.1
Etchevers, O.2
Paduano, J.D.3
Epstein, A.H.4
Hendricks, G.J.5
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16
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0034878791
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Compressor stability enhancement using discrete tip injection
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Suder, K.L., Hathaway, M.D., Thorp, S.A., Strazisar, A.J., Bright, M.B., 2001: Compressor Stability Enhancement Using Discrete Tip Injection, ASME J. of Turbomachinery, 123, pp. 14-23.
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(2001)
ASME J. of Turbomachinery
, vol.123
, pp. 14-23
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Suder, K.L.1
Hathaway, M.D.2
Thorp, S.A.3
Strazisar, A.J.4
Bright, M.B.5
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