Method for determining streamline flow pattern of nonviscous incompressible fluid about oblique airfoil from corresponding flow pattern about airfoil in normal position is presented and illustrated with two examples; method can be extended to account approximately for compressibility effects by applying Prandtl-Glauert correction factor to flow pattern that is normal to leading edge of airfoil.
Streamline pattern in vicinity of oblique airfoil
Nat Advisory Committee Aeronautics -- Tech Note
1947
7 pages
20 Supp Plates
Report
English
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