Leading-edge deflection optimization for a highly swept arrow-wing configuration /

Bibliographic Details
Main Authors:	Coe, Paul L. (Author), Huffman, Jarrett K. (Author), Fenbert, James W. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:	NASA technical paper ; 1777.
Subjects:	Aerodynamics. Airplanes > Wings, Swept-back. Leading edges (Aerodynamics)
Online Access:	https://purl.fdlp.gov/GPO/gpo71426

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