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

Main Author: Henderson, William P.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Series:NASA technical paper 1351
Subjects:
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100 1 |a Henderson, William P. 
245 1 0 |a Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44o swept wing/  |c William P. Hendersn 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Office,  |c 1978 
300 |a 35 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 1351 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Leading edges (Aerodynamics) 
650 0 |a Drag (Aerodynamics) 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Office 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Office 
710 2 |a Langley Research Center 
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