Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing /

Bibliographic Details

Main Author:	Henderson, William P.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1978.
Series:	NASA technical paper ; 1351.
Subjects:	Leading edges (Aerodynamics) Drag (Aerodynamics)