Results for cascades of airfoils as corresponds to case of impeller of axial propeller pump and propeller fan; lift and pressure drag coefficients on center section of 6, 7, and 9-section cascades are compared with results from tests of single airfoil. English translation from Soc Mech Engrs, Japan -- Trans v 3 n 12 Nov 1937.
Tests of cascades of airfoils for retarded flow
Nat Advisory Committee Aeronautics -- Tech Memo
1947
28 pages
Report
English
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