Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces /

Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces /

This report contains wind-tunnel results of the effect of change in horizontal-tail size and location on the static-lateral-stability parameters for a complete mode with wing and tail surfaces having the quarter-chord line swept back 45 degrees. Charts applicable to the design of similar tail config...

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Bibliographic Details
Main Author: Brewer, Jack D
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Lichtenstein, Jacob H
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1950
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2010
Subjects:
Airplanes > Models > Testing
Airplanes > Tail surfaces
Airplanes > Wings, Swept-back
Stability of airplanes, Lateral
Wind tunnel testing
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Stanford University

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Call Number: NACA TN 2010

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