Some effects of fuselage flexibility on longitudinal stability and control /

Some effects of fuselage flexibility on longitudinal stability and control / Bernard B. Klawans and Harold I. Johnson.

Some effects of fuselage flexibility on longitudinal stability and control of a large airplane are determined by application of a semirigid analytical technique. The dynamic characteristics are examined by studying the period and damping of the short-period longitudinal modes of oscillation of the f...

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Bibliographic Details
Main Author: Klawans, Bernard B.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Johnson, Harold I.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3543.
Subjects:
Airplanes > Fuselage.
Vibration (Aeronautics)
Aeroelasticity.
Airplanes > Control.
Stability of airplanes, Longitudinal.

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Call Number: Y 3.N 21/5:6/3543
Y 3.N 21/5:6/3543 Available Place a Hold

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