Tail-design requirements for satisfactory spin recovery /

A chart is presented that shows an empirical relationship between a tail-damping power factor and the relative density and mass distribution for satisfactory spin recovery. A formula for computing the tail-damping power factor is also given

Bibliographic Details
Main Author: Neihouse, A. I
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Lichtenstein, Jacob H, Pepoon, Philip W
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1946
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1045
Subjects:

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Stanford University

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Call Number: NACA TN 1045