메뉴 건너뛰기




Volumn 22, Issue 2, 2005, Pages 59-77

High-frequency pressure oscillations of rotating stall type. Part 1: Time and frequency characteristics

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; ROTORS; SENSORS; SHOCK WAVES; TURBOMACHINE BLADES;

EID: 18044388718     PISSN: 03340082     EISSN: None     Source Type: Journal    
DOI: 10.1515/TJJ.2005.22.2.59     Document Type: Article
Times cited : (4)

References (6)
  • 2
    • 0032979079 scopus 로고    scopus 로고
    • Stall inception and the prospects for active control in four high-speed compressors
    • Day, I.J., Breuer, T., Escuret, J., Cherrett, M., and Wilson, A., 1999, "Stall inception and the prospects for active control in four high-speed compressors". ASME J. of Turbomachinery, 121, pp. 18-27.
    • (1999) ASME J. of Turbomachinery , vol.121 , pp. 18-27
    • Day, I.J.1    Breuer, T.2    Escuret, J.3    Cherrett, M.4    Wilson, A.5
  • 3
    • 0342700197 scopus 로고    scopus 로고
    • Stall inception in the compressor system of a turbofan engine
    • Höss, B., Leinhos, D., and Fotter, L., 2000, "Stall inception in the compressor system of a turbofan engine". ASME J. of Turbomachinery, 122, pp. 32-44.
    • (2000) ASME J. of Turbomachinery , vol.122 , pp. 32-44
    • Höss, B.1    Leinhos, D.2    Fotter, L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.