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Volumn 119, Issue 1, 1997, Pages 31-38

Grid orthogonality effects on predicted turbine midspan heat transfer and performance

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; FINITE DIFFERENCE METHOD; FINITE VOLUME METHOD; HEAT TRANSFER; NAVIER STOKES EQUATIONS; PERFORMANCE; STATORS; THREE DIMENSIONAL; TURBOMACHINE BLADES;

EID: 0030935566     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841008     Document Type: Article
Times cited : (28)

References (18)
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  • 2
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  • 4
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    • (1978) Paper No. AIAA-78-257
    • Baldwin, B.S.1    Lomax, H.2
  • 5
    • 85006041218 scopus 로고
    • Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows
    • Boyle, R. J., and Giel, P. W., 1992, “Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows,” Paper No. AIAA-92-3068.
    • (1992) Paper No. AIAA-92-3068
    • Boyle, R.J.1    Giel, P.W.2
  • 6
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    • Chien, K.Y.1
  • 7
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    • Chima, R. V., 1987, “Explicit Multigrid Algorithm for Quasi-Three-Dimensional Flows in Turbomachinery,” AIAA Journal of Propulsion and Power, Vol. 3, No. 5, pp. 397-405.
    • (1987) Journal of Propulsion and Power , vol.3 , Issue.5 , pp. 397-405
    • Chima, R.V.1
  • 8
    • 0024090602 scopus 로고
    • Prediction of Compressor Cascade Performance Using a Navier-Stokes Technique
    • Davis, R. L., Hobbs D. E., and Weingold, H. D., 1988, “Prediction of Compressor Cascade Performance Using a Navier-Stokes Technique,” ASME Journal of Turbomachinery, Vol. 110, No. 4, pp. 520-531.
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  • 9
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  • 12
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  • 13
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  • 14
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  • 15
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  • 16
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.