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Volumn 123, Issue 3, 2001, Pages 534-543

A computation study of a novel turbine rotor partial shroud

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL METHODS; ROTORS; STEADY FLOW;

EID: 0035389531     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1370166     Document Type: Article
Times cited : (87)

References (52)
  • 9
    • 0004007504 scopus 로고
    • The effects of relative motion, blade edge radius and gap size on blade tip pressure distribution in an annular cascade with clearance
    • (1988) ASME 88-GT-256
    • Morphis, G.1    Bindon, J.P.2
  • 30
    • 0004168661 scopus 로고
    • Pressure distributions in the tip clearance region of an unshrouded axial turbine as affecting the problem of tip burnout
    • (1987) ASME 87-GT-230
    • Bindon, J.P.1
  • 33
    • 0024085153 scopus 로고
    • Analysis of rotor tip clearance loss in axial-flow turbines
    • (1988) J. Propulsion , vol.4 , Issue.5 , pp. 452-457
    • Farokhi, S.1
  • 41
    • 0019029698 scopus 로고
    • Exit plane and saction surface flows in an annular turbine cascade with a skewed inlet boundary layer
    • (1980) Int. J. Heat Fluid Flow , vol.2 , Issue.2 , pp. 57-66
    • Bindon, J.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.