메뉴 건너뛰기




Volumn 124, Issue 3, 2002, Pages 461-471

A converging slot-hole film-cooling geometry-Part 2: Transonic nozzle guide vane heat transfer and loss

Author keywords

[No Author keywords available]

Indexed keywords

COOLING; HEAT LOSSES; HEAT TRANSFER; LITHOGRAPHY; NOZZLES; REYNOLDS NUMBER; ROTORS; TRANSONIC AERODYNAMICS; TURBOMACHINE BLADES;

EID: 0036649767     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1459736     Document Type: Article
Times cited : (145)

References (35)
  • 13
    • 0032208652 scopus 로고    scopus 로고
    • Evaluating aerodynamic characteristics of wind-tunnel models produced by rapid prototyping methods
    • (1998) J. Spacecr. Rockets , vol.35 , Issue.6
    • Springer, A.1
  • 17
  • 35
    • 0015143343 scopus 로고
    • Konsistente Mittelwerte in der Theorie der Turbomaschinen fur Kompressible Medien
    • (1971) BBC-Mitt , vol.58 , pp. 485-492
    • Dzung, L.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.