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

Bibliographic Details
Main Author:	Coe, Paul L.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors:	Huffman, Jarrett K., Fenbert, James W.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va. : For sale by the National Technical Information Service], National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980.
Series:	NASA technical paper ; 1777.
Subjects:	Aerodynamics. Airplanes > Wings, Swept-back. Leading edges (Aerodynamics)