Due to increased interest in design of fans and turbines procedure is presented for obtaining pressure distribution on arbitrary airfoil section in cascade in two-dimensional, incompressible, and nonviscous flow. (published 1949) (15¢)
Interference method for obtaining potential flow past arbitrary cascade of airfoils
Nat Advisory Committee Aeronautics -- Report
1947
18 pages
Report
English
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Interference method for obtaining potential flow past arbitrary cascade of airfoils
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