NASA NTRS · 19820005240
Computational methods for internal flows with emphasis on turbomachinery
Abstract
Current computational methods for analyzing flows in turbomachinery and other related internal propulsion components are presented. The methods are divided into two classes. The inviscid methods deal specifically with turbomachinery applications. Viscous methods, deal with generalized duct flows as well as flows in turbomachinery passages. Inviscid methods are categorized into the potential, stream function, and Euler aproaches. Viscous methods are treated in terms of parabolic, partially parabolic, and elliptic procedures. Various grids used in association with these procedures are also discussed.
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Mcnally, W. D., Sockol, P. M.. 1981-01-01. Computational methods for internal flows with emphasis on turbomachinery. https://ntrs.nasa.gov/citations/19820005240
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