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Volumn 128, Issue 1, 2006, Pages 20-28

Experimental operating range extension of a twin-spool turbofan engine by active stability control measures

Author keywords

[No Author keywords available]

Indexed keywords

AIR ENTRAINMENT; AIRCRAFT; CONTROL SYSTEMS; REAL TIME SYSTEMS; ROTORS; SYSTEM STABILITY;

EID: 33645793497     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2031247     Document Type: Article
Times cited : (14)

References (17)
  • 1
    • 0032703439 scopus 로고    scopus 로고
    • "Rotating Stall Control In A High-Speed Stage With Inlet Distortion, Part I-Radial Distortion"
    • "Part II-Circumferential Distortion," Pract. Period. Hazard., Toxic, Radioact. Waste Manage., pp. 517-524
    • Spakovszky, Z. S., Weigl, H. J., Paduano, J. D., van Schalkwyk, C. M., Suder, K. L., and Bright, M. M., 1999, "Rotating Stall Control In A High-Speed Stage With Inlet Distortion, Part I-Radial Distortion," Pract. Period. Hazard., Toxic, Radioact. Waste Manage. 121, pp. 510-516,, "Part II-Circumferential Distortion," Pract. Period. Hazard., Toxic, Radioact. Waste Manage., pp. 517-524.
    • (1999) Pract. Period. Hazard., Toxic, Radioact. Waste Manage. , vol.121 , pp. 510-516
    • 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
  • 5
    • 33645768775 scopus 로고    scopus 로고
    • "Active Stabilization of a Low-Pressure Compressor in a Turbofan Engine With Constant Air Injection"
    • Proc., AIAA-2001-3312
    • Leinhos, D. C., Scheidler, S., and Fottner, L., 2001, "Active Stabilization of a Low-Pressure Compressor in a Turbofan Engine With Constant Air Injection," Proc., AIAA-2001-3312.
    • (2001)
    • Leinhos, D.C.1    Scheidler, S.2    Fottner, L.3
  • 13
    • 10244269023 scopus 로고    scopus 로고
    • "Operational Characteristics of a Twin-Spool Turbofan Engine at Inlet Distortions With Reduced Surge Margin"
    • RTO-AVT-100-029, RTO-AVT-100
    • Scheidler, S. G., and Fottner, L. 2003, "Operational Characteristics of a Twin-Spool Turbofan Engine at Inlet Distortions With Reduced Surge Margin," Proc. Symposium on Vehicle Propulsion Integration, RTO-AVT-100-029, RTO-AVT-100.
    • (2003) Proc. Symposium on Vehicle Propulsion Integration
    • Scheidler, S.G.1    Fottner, L.2
  • 14
    • 0034877484 scopus 로고    scopus 로고
    • "The Influence of Transient Inlet Distortions on The Instability Inception of a Low Pressure Compressor in a Turbofan Engine"
    • Leinhos, D. C., Schmid, N. R., and Fottner, L., 2001, "The Influence of Transient Inlet Distortions on The Instability Inception of a Low Pressure Compressor in a Turbofan Engine," Pract. Period. Hazard., Toxic, Radioact. Waste Manage. 123, pp. 1-8.
    • (2001) Pract. Period. Hazard., Toxic, Radioact. Waste Manage. , vol.123 , pp. 1-8
    • Leinhos, D.C.1    Schmid, N.R.2    Fottner, L.3
  • 15
    • 33645785108 scopus 로고
    • "A System for Monitoring, Measurement, and Analysis of Transient Performance and Stall Phenomena of Gas Turbine Engines"
    • IEEE, New York, IEEE Publication 93CH3199-7
    • Herpel, Th., and Fottner, L., 1993, "A System for Monitoring, Measurement, and Analysis of Transient Performance and Stall Phenomena of Gas Turbine Engines," Proc. ICIASF '93 Record, IEEE, New York, IEEE Publication 93CH3199-7.
    • (1993) Proc. ICIASF '93 Record
    • Herpel, Th.1    Fottner, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.