Low-speed aerodynamic characteristics of a 17-percent-thick airfoil section designed for general aviation applications /

"An investigation was conducted in the Langley low-turbulence pressure tunnel to determine the low-speed two-dimensional aerodynamic characteristics of a 17-percent thick airfoil designed for general aviation applications. The results are compared with a typical older NACA 65 series airfoil sec...

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Bibliographic Details
Main Author: McGhee, Robert J
Corporate Authors: United States National Aeronautics and Space Administration, Langley Research Center
Other Authors: Beasley, William D
Format: Book
Language:English
Published: Washington D.C. : Alexandria, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1973
Washington D.C. : [Springfield, Virg. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service], 1973
Series:NASA Technical Note ; D-7428
NASA technical note ; D-7428
Subjects:

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Call Number: NASA TN D-7428

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Call Number: NASA TN D-7428