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Volumn 120, Issue 1, 1998, Pages 63-69

Heat transfer measurements to a gas turbine cooling passage with inclined ribs

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COOLING; GAS TURBINE; HEAT TRANSFER; VORTEX;

EID: 0031924015     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841390     Document Type: Article
Times cited : (60)

References (17)
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    • Ireland, P.T.1    Wang, Z.2    Jones, T.V.3
  • 8
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  • 10
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    • (1990) Int. Journal of Heat and Mass Transfer , vol.33 , Issue.11 , pp. 2439-2449
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  • 11
    • 4243062930 scopus 로고    scopus 로고
    • Heat Transfer Enhancement Within a Turbine Blade Cooling Passage Using Ribs and Combinations of Ribs With Film Cooling Holes
    • Shen, J. R., Ireland, P. T., Wang, Z., Jones, T. V., and Byerley, A. R., 1996, “Heat Transfer Enhancement Within a Turbine Blade Cooling Passage Using Ribs and Combinations of Ribs With Film Cooling Holes,” ASME Journal of Turbomachinery, Vol. 118, pp. 428-434.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.