Full potential solution of transonic quasi-three-dimensional flow through a cascade using artificial compressibility
Journal Article
·
· J. Eng. Power; (United States)
A reliable method is presented for calculating the flowfield about a cascade of arbitrary two-dimensional airfoils. The method approximates the three-dimensional flow in a turbomachinery blade row by correcting for streamtube convergence and radius change in the throughflow direction. 12 refs.
- Research Organization:
- NASA, Lewis Res Cent, Cleveland, Ohio, USA
- OSTI ID:
- 5224302
- Journal Information:
- J. Eng. Power; (United States), Vol. 104:1
- Country of Publication:
- United States
- Language:
- English
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