Influence of nonlinear effects on flight behavior of high-performance aircraft under control inputs is demonstrated with systematic calculations showing coupling effects with various symmetrical and unsymmetrical control inputs at different Mach numbers and altitudes; effects of changing aerodynamic derivatives, engine gyroscopic couple, and ratio of moments of inertia are demonstrated.
Influence of deflection of control surfaces on free-flight behaviour of aeroplane
AGARD -- Report
1961
22 pages
Report
English
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