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Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation

By Pittman, J. L.

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Book Id: WPLBN0002206898
Format Type: PDF eBook :
File Size: 14.1 MB
Reproduction Date: 2012
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Title: Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation  
Author: Pittman, J. L.
Volume:
Language: English
Subject: ANALYZERS, CARBON, ENGINEERING DRAWINGS
Collections: NASA Publication Collection
Historic
Publication Date:
1984
Publisher:

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L, P. J., H, M. W., & S, M. D. (1984). Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation. Retrieved from http://nationalpubliclibrary.info/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Results of the experimental validation are presented for the three dimensional cambered wing which was designed to achieve attached supercri

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: ANALYZERS; CARBON; ENGINEERING DRAWINGS; CALIBRATING; EQUIPMENT SPECIFICATIONS; ULTRAVIOLET ABSORPTION; FAILURE MODES

 

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