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    Validation of viscous and inviscid computational methods for turbomachinery components (1986)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An assessment of several three-dimensional computer codes used at the NASA Lewis Research Center is presented. Four flow situations are examined, for which both experimental data and computational results are available. The four flows form a basis for the evaluation of the computational procedures. It is concluded that transonic rotor flow at peak efficiency conditions may be calculated with a reasonable degree of accuracy, whereas, off-design conditions are not accurately determined. Duct flows and turbine cascade flows may also be computed with reasonable accuracy whereas radial inflow turbine flow remains a challenging problem.
    Keywords: AERODYNAMICS
    Type: NASA-TM-87193 , E-2765 , NAS 1.15:87193 , International Gas Turbine Conference; Dusseldorf; Germany
    Format: application/pdf
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