Cover Image

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
Description
Item Description:Title from title screen (viewed on Aug. 25, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (56 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 55-56).