Effect of leading-edge load constraints on the design and performance of supersonic wings/

Main Author: Darden, Christine M.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
Series:NASA technical paper 2446
Subjects:
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100 1 |a Darden, Christine M. 
245 1 0 |a Effect of leading-edge load constraints on the design and performance of supersonic wings/  |c Christine M. Darden 
246 1 3 |a Effect of leading edge load constraints on the design and performance of supersonic wings 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1985 
300 |a 74 Σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 2446 
650 0 |a Airplanes  |x Wings 
650 0 |a Aerodynamics, Supersonic 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
710 2 |a Langley Research Center 
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