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Effects of unsymmetrical air-flow characteristics of twin-intake air-induction systems on airplane static stability at supersonic speeds

By Anderson, W. E.

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Book Id: WPLBN0002201556
Format Type: PDF eBook:
File Size: 9.39 MB
Reproduction Date: 2012



Title: Effects of unsymmetrical air-flow characteristics of twin-intake air-induction systems on airplane static stability at supersonic speeds  
Author: Anderson, W. E.
Volume:
Language: English
Subject: FLAT PLATES, LAMINAR BOUNDARY LAYER, LEADING EDGES
Collections: Space and Aviation eDocuments Collection, NASA Publication Collection
Historic
Publication Date:
1959
Publisher:

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W. E, B. A., & W, P. E. (1959). Effects of unsymmetrical air-flow characteristics of twin-intake air-induction systems on airplane static stability at supersonic speeds. Retrieved from https://self.gutenberg.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents

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: FLAT PLATES; LAMINAR BOUNDARY LAYER; LEADING EDGES; APPROXIMATION; ROTATING BODIES; THREE DIMENSIONAL BOUNDARY LAYER; MATHEMATICAL MODELS; VELOCITY DISTRIBUTION

 
 



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