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Volumn 375, Issue 1, 2004, Pages 639-649

Adiabatic effectiveness measurements and predictions of leakage flows along a blade endwall

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTORS; COMPRESSED AIR; COMPUTATIONAL METHODS; COOLING; HIGH PRESSURE EFFECTS; TURBOMACHINE BLADES; WIND TUNNELS;

EID: 20344393905     PISSN: 02725673     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2004-62021     Document Type: Conference Paper
Times cited : (5)

References (16)
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  • 2
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  • 3
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  • 4
    • 0024107705 scopus 로고
    • Turbulent transport on the endwall in the region between adjacent turbine blades
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  • 5
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    • Heat transfer and flowfield measurements in the leading edge region of a stator vane endwall
    • Kang, M.B., Kohli, A., and Thole, K.A., 1999 "Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall," J of Turbomachinery, 121, pp. 558-568.
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  • 6
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    • An experimental study of heat transfer and film cooling on large-scale turbine endwall
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    • (1974) ASME J of Heat Transfer , vol.96 , pp. 524-529
    • Blair, M.F.1
  • 8
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    • Combustor turbine interface studies - Part 1: Endwall effectiveness measurements
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  • 9
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  • 10
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  • 12
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  • 13
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  • 15
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.