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Volumn 123, Issue 4, 2001, Pages 645-654

Film cooling of a cylindrical leading edge with injection through rows of compound-angle holes

Author keywords

Computational; Film cooling; Heat transfer; Turbines; Turbulence

Indexed keywords

COOLING; FILMS; JETS; SHEAR STRESS; SURFACE PROPERTIES; TEMPERATURE DISTRIBUTION; WALL FLOW;

EID: 0035423046     PISSN: 00221481     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1370513     Document Type: Article
Times cited : (55)

References (32)
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  • 6
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    • Ou, S.1    Han, J.C.2
  • 9
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    • Aspects of vane film cooling with high turbulence: Part I-Heat transfer
    • (1998) ASME J. Turbomach , vol.120 , pp. 768-776
    • Ames, F.E.1
  • 10
    • 0032194331 scopus 로고    scopus 로고
    • Aspects of vane film cooling with high turbulence: Part II-Adiabatic effectiveness
    • (1998) ASME J. Turbomach , vol.120 , pp. 777-784
    • Ames, F.E.1
  • 26
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    • Approximate riemann solvers, parameter vector and difference schemes J
    • (1981) Comput. Phys , vol.43 , pp. 357-372
    • Roe, P.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.