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Volumn 934, Issue , 2001, Pages 147-161

Jet-impingement heat transfer in gas turbine systems

Author keywords

[No Author keywords available]

Indexed keywords

CONFERENCE PAPER; COOLING; FLOW RATE; GAS FLOW; HEAT TRANSFER; JET INJECTION; ROTATION; SURFACE PROPERTY; TURBULENT FLOW;

EID: 0034953282     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05849.x     Document Type: Conference Paper
Times cited : (274)

References (80)
  • 48
    • 0023454041 scopus 로고
    • Impingement heat transfer within arrays of circular jets - Part i. Effects of minimum, intermediate, and complete crossflow for small and large spacings
    • (1987) J. Heat Transfer , vol.107 , pp. 872-879
    • Obot, N.T.1    Trabold, T.A.2
  • 57
    • 0025465227 scopus 로고
    • Local heat transfer in internally cooled turbine airfoil leading edge regions: Part II - Impingement cooling with film coolant extraction
    • (1990) J. Turbomachinery , vol.112 , pp. 459-466
    • Metzger, D.E.1    Bunker, R.S.2
  • 58
    • 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) J. Eng. Power , vol.92 , pp. 1970
    • Kercher, D.M.1    Tabakoff, W.2
  • 65
    • 0029159192 scopus 로고
    • Heat transfer and flow characteristics of an oblique turbulent impinging jet within confined walls
    • (1995) J. Heat Transfer , vol.117 , pp. 316-322
    • Ichimiya, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.