Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
By: William P. Hendersn, Langley Research Center.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Langley Research Center.
Series: NASA technical paper ; 1351; NASA technical paper -- 1351.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 35
Subjects: Leading edges (Aerodynamics); Drag (Aerodynamics)
Notes: Nov. 1978.

Includes bibliographical references.