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NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel/

Main Author:	Jenkins, Renaldo V.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989
Series:	NASA technical paper 2890
Subjects:	Aerofoils

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