Charts for estimation of longitudinal-stability derivatives for a helicopter rotor in forward flight /

Charts are presented that provide a convenient means for obtaining the longitudinal-stability derivatives (except those with respect to pitching velocity) of a helicopter rotor in forward flight. These charts do not rely upon the often-used assumption that the rotor resultant-force vector is perpend...

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Bibliographic Details
Main Author: Amer, Kenneth B
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Gustafson, F. B
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2309
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Stanford University

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Call Number: NACA TN 2309