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Volumn 123, Issue 1, 2001, Pages 147-153

An experimental evaluation of advanced leading edge impingement cooling concepts

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; GEOMETRY; REYNOLDS NUMBER; SURFACE ROUGHNESS; WALLS (STRUCTURAL PARTITIONS);

EID: 0034864192     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1331537     Document Type: Article
Times cited : (135)

References (30)
  • 20
    • 84970871114 scopus 로고
    • Heat transfer by a square array of round air jets impinging perpendicular to a flat surface including the effect of spent air
    • (1970) ASME J. Eng. Power , vol.92 , Issue.1 , pp. 73-82
    • Kercher, D.M.1    Tabakoff, W.2
  • 24
    • 0025465227 scopus 로고
    • Local heat transfer in internally cooled turbine airfoil leading edge regions: Part II-impingement cooling with film coolant extraction
    • (1990) ASME J. Turbomach , vol.112 , Issue.3 , pp. 459-466
    • Bunker, R.S.1    Metzger, D.E.2
  • 25
    • 0025460721 scopus 로고
    • Local heat transfer in internally cooled turbine airfoil leading edge regions: Part I-impingement cooling without film coolant extraction
    • (1990) ASME J. Turbomach , vol.112 , pp. 451-458
    • Metzger, D.E.1    Bunker, R.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.