For the case of flutter analysis, lift history for the motion obtained from the Wagner analysis ( Herbert A . Wagner ) with varying frequency of oscillation shows that magnitude of lift decreases and a phase lag develops between the aircraft motion and the unsteady aerodynamic forces.
22.
The amplitude of the color signal represents the saturation of the color and the phase lag of the color signal with respect to a certain reference which is called colorburst represents the hue; i . e ., each phase lag is assigned for a different color hue.
23.
The amplitude of the color signal represents the saturation of the color and the phase lag of the color signal with respect to a certain reference which is called colorburst represents the hue; i . e ., each phase lag is assigned for a different color hue.
24.
In the aerodynamics of rotorcraft such as helicopters, "'phase lag "'refers to the angular difference between the point at which a control input to a rotor blade occurs and the point of maximum displacement of the blade in response to that control input, said displacement occurring in the direction of rotor rotation . " Phase lag " differs from " advance angle " in that the latter refers to the mechanically fixed angle between the pitch link attachments at the blade and swashplate . " Phase lag " can vary as a function on rotor tilt rate and aerodynamic damping and results in " cross-coupling " between the aircraft control axes; " advance angle " is fixed and cannot vary.
25.
In the aerodynamics of rotorcraft such as helicopters, "'phase lag "'refers to the angular difference between the point at which a control input to a rotor blade occurs and the point of maximum displacement of the blade in response to that control input, said displacement occurring in the direction of rotor rotation . " Phase lag " differs from " advance angle " in that the latter refers to the mechanically fixed angle between the pitch link attachments at the blade and swashplate . " Phase lag " can vary as a function on rotor tilt rate and aerodynamic damping and results in " cross-coupling " between the aircraft control axes; " advance angle " is fixed and cannot vary.
26.
In the aerodynamics of rotorcraft such as helicopters, "'phase lag "'refers to the angular difference between the point at which a control input to a rotor blade occurs and the point of maximum displacement of the blade in response to that control input, said displacement occurring in the direction of rotor rotation . " Phase lag " differs from " advance angle " in that the latter refers to the mechanically fixed angle between the pitch link attachments at the blade and swashplate . " Phase lag " can vary as a function on rotor tilt rate and aerodynamic damping and results in " cross-coupling " between the aircraft control axes; " advance angle " is fixed and cannot vary.
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