메뉴 건너뛰기




Volumn 65, Issue 8, 2000, Pages 217-224

Endwall boundary layer separation in a single-stage axial-flow low-speed compressor and a high-stagger compressor cascade;Abgelöste seitenwandgrenzschichten in einem einstufigen axialverdichter und in einem hochgestaffelten verdichtergitter

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; OIL WELL CASINGS; REYNOLDS NUMBER; ROTORS; SPEED;

EID: 0040792532     PISSN: 00157899     EISSN: None     Source Type: Journal    
DOI: 10.1007/s100109900019     Document Type: Article
Times cited : (20)

References (31)
  • 3
    • 0023307160 scopus 로고
    • Pressure losses and flow field distortion induced by tip clearance of centrifugal and axial compressors
    • Senoo Y (1987) Pressure losses and flow field distortion induced by tip clearance of centrifugal and axial compressors. JSME International Journal 30, No. 261, 375-385
    • (1987) JSME International Journal , vol.30 , Issue.261 , pp. 375-385
    • Senoo, Y.1
  • 4
    • 0003747148 scopus 로고
    • Published by Longman Scientific and Technical
    • Cumpsty NA (1989) Compressor Aerodynamics. Published by Longman Scientific and Technical
    • (1989) Compressor Aerodynamics
    • Cumpsty, N.A.1
  • 5
    • 0002639026 scopus 로고
    • Casing boundary layers in multistage axial-flow compressors
    • Elsevier, Amsterdam
    • Smith LH (1970) Casing boundary layers in multistage axial-flow compressors. Flow Research on Blading, Elsevier, Amsterdam
    • (1970) Flow Research on Blading
    • Smith, L.H.1
  • 7
    • 0019622405 scopus 로고
    • Stalling pressure rise capability of axial flow compressor stages
    • Koch CC (1981) Stalling pressure rise capability of axial flow compressor stages. ASME Journal of Engineering for Power 103, 645-656
    • (1981) ASME Journal of Engineering for Power , vol.103 , pp. 645-656
    • Koch, C.C.1
  • 12
    • 0001722651 scopus 로고
    • Loss and stall analysis of compressor cascades
    • Lieblein S (1959) Loss and stall analysis of compressor cascades. ASME Journal of Basic Engineering 81, No. 3, 387-400
    • (1959) ASME Journal of Basic Engineering , vol.81 , Issue.3 , pp. 387-400
    • Lieblein, S.1
  • 13
    • 85013814204 scopus 로고    scopus 로고
    • Incidence and deviation-angle correlations for compressor cascades
    • 196
    • Lieblein S (196) Incidence and deviation-angle correlations for compressor cascades. ASME Journal of Basic Engineering 82, No. 3, 575-587
    • ASME Journal of Basic Engineering , vol.82 , Issue.3 , pp. 575-587
    • Lieblein, S.1
  • 14
    • 0039594150 scopus 로고
    • Das verhalten von tragflügelgittern in axialverdichtern und im windkanal
    • de Haller P (1953) Das Verhalten von Tragflügelgittern in Axialverdichtern und im Windkanal. Brennstoff-Wärme-Kraft (BWK) 5, 333-336
    • (1953) Brennstoff-wärme-kraft (BWK) , vol.5 , pp. 333-336
    • De Haller, P.1
  • 15
    • 0042635994 scopus 로고
    • Discussion to Benser WA: Transonic compressor technology advancements
    • NASA SP-304
    • Koch CC (1974) Discussion to Benser WA: Transonic compressor technology advancements. Fluid mechanics, Acoustics, and Design of Turbomachinery, Part II, NASA SP-304
    • (1974) Fluid Mechanics, Acoustics, and Design of Turbomachinery , Issue.PART II
    • Koch, C.C.1
  • 16
    • 0006798264 scopus 로고
    • Ph. D. thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology
    • Chen GT (1991) Vortical structures in turbomachinery tip clearance flows. Ph. D. thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology
    • (1991) Vortical Structures in Turbomachinery Tip Clearance Flows
    • Chen, G.T.1
  • 18
    • 0003808462 scopus 로고    scopus 로고
    • Ph. D. thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology
    • Khalsa AS (1996) Endwall blockage in axial compressors. Ph. D. thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology
    • (1996) Endwall Blockage in Axial Compressors
    • Khalsa, A.S.1
  • 19
    • 0024702584 scopus 로고
    • Structure of tip clearance flow in an isolated axial compressor rotor
    • Inoue M, Kuroumaru M (1989) Structure of tip clearance flow in an isolated axial compressor rotor. ASME Journal of Turbomachinery 111, No. 2, 250-256
    • (1989) ASME Journal of Turbomachinery , vol.111 , Issue.2 , pp. 250-256
    • Inoue, M.1    Kuroumaru, M.2
  • 20
    • 0020190817 scopus 로고
    • Casing wall boundary layer development through an isolated compressor rotor
    • Hunter IH, Cumpsty NA (1982) Casing wall boundary layer development through an isolated compressor rotor. ASME Journal of Engineering for Power 104, No. 4, 805-817
    • (1982) ASME Journal of Engineering for Power , vol.104 , Issue.4 , pp. 805-817
    • Hunter, I.H.1    Cumpsty, N.A.2
  • 21
    • 0039001424 scopus 로고
    • An analysis of axial compressor cascade aerodynamics. Parts I and II
    • Mellor GL (1959) An analysis of axial compressor cascade aerodynamics. Parts I and II. ASME Journal of Basic Engineering 81, No. 3, 362-386
    • (1959) ASME Journal of Basic Engineering , vol.81 , Issue.3 , pp. 362-386
    • Mellor, G.L.1
  • 22
  • 24
  • 26
    • 0040779865 scopus 로고    scopus 로고
    • Sekundärströmungen in einem hoch gestaffelten verdichtergitter mit spalt
    • Berlin, Germany
    • Homeier L, Saathoff H (1999) Sekundärströmungen in einem hoch gestaffelten Verdichtergitter mit Spalt. To be presented at the DGLR-Jahrestagung 1999, Berlin, Germany
    • (1999) DGLR-Jahrestagung 1999
    • Homeier, L.1    Saathoff, H.2
  • 27
    • 0026143132 scopus 로고
    • Detection of a rotating stall precursor in isolated axial flow compressor rotors
    • Inoue M, Kuroumaru M, Iwamoto T, Ando Y (1991) Detection of a rotating stall precursor in isolated axial flow compressor rotors. ASME Journal of Turbomachinery 113, No. 2, 282-289
    • (1991) ASME Journal of Turbomachinery , vol.113 , Issue.2 , pp. 282-289
    • Inoue, M.1    Kuroumaru, M.2    Iwamoto, T.3    Ando, Y.4
  • 29
    • 0040779862 scopus 로고    scopus 로고
    • Stall margin improvement using circumferential high-speed fluid injection
    • Honolulu, Hawaii, USA
    • Goto A (1998) Stall margin improvement using circumferential high-speed fluid injection. Proceedings of ISROMAC-7, Honolulu, Hawaii, USA, 1123-1138
    • (1998) Proceedings of ISROMAC-7 , pp. 1123-1138
    • Goto, A.1
  • 30
    • 84939175125 scopus 로고
    • Part-circumference casing treatment and the effect on compressor stall
    • Toronto, Canada
    • Cumpsty NA (1989) Part-circumference casing treatment and the effect on compressor stall. Paper 89-GT-312 presented at the Gas Turbine & Aeroengine Congress & Exposition, Toronto, Canada
    • (1989) Gas Turbine & Aeroengine Congress & Exposition
    • Cumpsty, N.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.