메뉴 건너뛰기




Volumn 123, Issue 4, 2001, Pages 675-681

Effects of rib arrangements on heat transfer and flow behavior in a rectangular rib-roughened passage: Application to cooling of gas turbine blade trailing edge

Author keywords

Cooling; Flow; Heat transfer; Thermocouples; Visualization

Indexed keywords

FLOW MEASUREMENT; FLOW VISUALIZATION; GAS TURBINES; PRESSURE DROP; TURBOMACHINE BLADES;

EID: 0035421440     PISSN: 00221481     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1378019     Document Type: Article
Times cited : (102)

References (26)
  • 2
    • 0026049023 scopus 로고
    • An experimental investigation of heat transfer coefficients in a spanwise rotating channel with two opposite rib-roughened walls
    • (1991) ASME J. Turbomach , vol.113 , pp. 75-82
    • Taslim, M.E.1
  • 10
    • 0030477397 scopus 로고    scopus 로고
    • Local heat transfer in rotating smooth and ribbed two-pass square channels with three channel orientations
    • (1996) ASME J. Turbomach , vol.118 , pp. 584-587
    • Dutta, S.1    Han, J.-C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.