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Volumn 124, Issue 1, 2002, Pages 52-60

Clocking effects in a 1.5 stage axial turbine-steady and unsteady experimental investigations supported by numerical simulations

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ASPECT RATIO; FLOW INTERACTIONS; OPTIMIZATION; ROTORS; STATORS; UNSTEADY FLOW; VISCOUS FLOW; WAKES;

EID: 0036191026     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1425811     Document Type: Article
Times cited : (93)

References (30)
  • 5
    • 0027982743 scopus 로고
    • A numerical study of the interaction of a transonic compressor rotor overtip leakage vortex with the following stator blade row
    • (1994) ASME Paper No. 94-GT-156
    • Dawes, W.N.1
  • 7
    • 0004130785 scopus 로고
    • UNSFLO: A numerical method for the calculating of unsteady flow in turbomachinery
    • MIT Gas Turbine Laboratory
    • (1991) GTL Report No. 205
    • Giles, M.B.1
  • 24
    • 0019999091 scopus 로고
    • Predictions of channel and boundary-layer flows with a low-reynolds-number turbulence model
    • (1982) AIAA J , vol.20 , Issue.1 , pp. 33-38
    • Chien, K.-Y.1
  • 30
    • 85136409960 scopus 로고
    • The effect of wakes on the transient pressure and velocity distribution in turbomachines
    • (1958) ASME J. Basic Eng , vol.80 , pp. 1544-1552
    • Meyer, R.N.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.