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Volumn 122, Issue 4, 2000, Pages 692-698

Time-averaged heat flux for a recessed tip, lip, and platform of a transonic turbine blade

Author keywords

[No Author keywords available]

Indexed keywords

BLADE; HEAT FLUX; TRANSONIC FLOW; TURBINE;

EID: 0034529709     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1311285     Document Type: Conference Paper
Times cited : (85)

References (28)
  • 1
    • 0024700755 scopus 로고
    • The influence of turbine clearance gap leakage on passage velocity and heat transfer near blade tips: Part I-Sink flow effects on blade pressure side
    • (1989) ASME J. Turbomach. , vol.111 , pp. 284-292
    • Metzger, D.E.1    Rued, K.2
  • 2
    • 0024699859 scopus 로고
    • The influence of turbine clearance gap leakage on passage velocity and heat transfer near blade tips: Part II-Source flow effects on blade suction sides
    • (1989) ASME J. Turbomach. , vol.111 , pp. 293-300
    • Metzger, D.E.1    Rued, K.2
  • 10
    • 85040886288 scopus 로고
    • Pressure and flowfield measurements of axial turbine tip clearance flow in a linear cascade
    • Cambridge University Engineering Department, TR 123
    • (1986)
    • Bindon, J.P.1
  • 11
    • 0003854511 scopus 로고
    • Visualization studies of secondary flows in turbine rotor tip regions
    • NACA TN 3519
    • (1955)
    • Allen, H.W.1    Kofskey, M.G.2
  • 15
    • 0034177995 scopus 로고    scopus 로고
    • Heat transfer and flow on the first stage blade tip of a power generation gas turbine, Part 1: Experimental results
    • NASA TM 1999-209152
    • (1999)
    • Bunker, R.S.1    Bailey, J.C.2    Ameri, A.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.