Leading-edge deflection optimization for a highly swept arrow-wing configuration
By: Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert
Contributors: Huffman, Jarrett K; Fenbert, James W; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1777
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va. : For sale by the National Technical Information Service]
Language: eng
Number of pages: 56
Subjects: Aerodynamics; Airplanes -- Wings, Swept-back; Leading edges (Aerodynamics)
Notes: "Langely Research Center, Hampton, Virginia."

Dec. 1980

Includes bibliographial references