The Streamline Pattern in the Vicinity of an Oblique Airfoil

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Summary: A method for determining the streamwise flow pattern of a nonviscous incompressible fluid about an oblique airfoil from the corresponding flow pattern about the airfoil in normal position is presented and illustrated in two examples. The method can be extended to account approximately for compressibility effects by applying the Prandtl-Glauert correction factor to the flow pattern that is normal to the leading edge of the airfoil. The method is expected to be useful in determining the shape of a fuselage or nacelle having a minimum of interference with the flow over a swept-back wing.
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930081869.
Accession ID: 93R11159.
NACA-TN-1231.
Terms of Use and Reproduction: No Copyright.

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