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JSME International Journal, Series B: Fluids and Thermal Engineering

Volumn 44, Issue 1, 2001, Pages 99-110

Enhancement of film cooling performance using a shaped film cooling hole with compound angle injection

(3) Cho, H H a Rhee, D H a Kim, B G a

a Department of Mechanical Engineering ^* (South Korea)

Author keywords

Compound angle injection; Film cooling; Gas turbine; Naphthalene sublimation method; Shaped film cooling hole

Indexed keywords

COOLANTS; DIFFUSION; HEAT TRANSFER COEFFICIENTS; MASS TRANSFER; NAPHTHALENE; SUBLIMATION;

FILM COOLING;

HEAT TRANSFER;

FILM COOLING; GAS TURBINE; HEAT TRANSFER ENHANCEMENT;

EID: 0035242982 PISSN: 13408054 EISSN: None Source Type: Journal
DOI: 10.1299/jsmeb.44.99 Document Type: Article

Times cited : (64)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.