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  • 1
    Publication Date: 2013-08-31
    Description: A steady, three-dimensional average-passage equation system is derived for use in simulating multistage turbomachinery flows. These equations describe a steady, viscous flow that is periodic from blade passage to blade passage. From this system of equations, various reduced forms can be derived for use in simulating the three-dimensional flow field within multistage machinery. It is suggested that a properly scaled form of the average-passage equation system would provide an improved mathematical model for simulating the flow in multistage machines at design and, in particular, at off-design conditions.
    Keywords: AERODYNAMICS
    Type: NASA-TM-86869 , NAS 1.15:86869 , E-2291
    Format: application/pdf
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