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Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50

By Church, J. D

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Book Id: WPLBN0002198607
Format Type: PDF eBook :
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Reproduction Date: 2012
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Title: Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50  
Author: Church, J. D
Volume:
Language: English
Subject: AIRCRAFT MODELS, SWEPT WINGS, SWEPT WING
Collections: NASA Publication Collection
Historic
Publication Date:
21655
Publisher:

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D, C. J. (21655). Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50. Retrieved from http://members.worldlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudinal and lateral stability and control char

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: AIRCRAFT MODELS; SWEPT WINGS; SWEPT WING; STATIC STABILITY AND CONTROL; DRAG MEASUREMENT; FIGHTER AIRCRAFT; WIND TUNNEL STABILITY TEST; WIND TUNNEL TESTS; WIND TUNNEL STABILITY TESTS; DRAG; DRAG MEASUREMENT; FIGHTER AIRCRAFT; LATERAL CONTROL; LATERAL STABILITY

 

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