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The Streamline Pattern in the Vicinity of an Oblique Airfoil

Charles E. Watkins

出版	National Advisory Committee for Aeronautics, 1947
URL	http://books.google.com.hk/books?id=VY7wPAAACAAJ&hl=&source=gbs_api

註釋

A method for determining the streamline flow pattern of a nonviscous incompressible fluid about an oblique airfoil from the corresponding flow pattern about the air in normal position is presented and illustrated with 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.