Phase lag ( rotorcraft ) will cause the extra lift to be seen approximately 90 degrees later in rotor rotation in semi-rigid two bladed rotor systems.
12.
For systems that are hinged at some distance from the axis of rotation ( such as a fully articulated rotor head ) the phase lag is less than 90 degrees.
13.
As a consequence of the phase lag, to turn the rotorcraft to the left or right would theoretically require a forward or backward cyclic if there was no mechanical correction.
14.
Rich notes, " His skillful use of gradual phase lag has led to some of his major achievements, bringing great beauty and expressiveness to his music ."
15.
Reduced frequency can be used to explain the amplitude attenuation and the phase lag of the unsteady aerodynamic forces compared to the quasi steady analysis ( which in theory assumes no phase lag ).
16.
Reduced frequency can be used to explain the amplitude attenuation and the phase lag of the unsteady aerodynamic forces compared to the quasi steady analysis ( which in theory assumes no phase lag ).
17.
The phase value is usually taken to be between-180 degrees and 0 ( that is, it represents a phase lag, for both positive and negative values of the arctan's argument ).
18.
However, only limited NFB can be used around the transformer, as there is phase lag caused by the transformer, and this causes instability if NFB is incorrectly ( without any phase / frequency correction ) used.
19.
Taking that as the definition of the transfer function requires careful disambiguation between complex vs . real values, which is traditionally influenced by the interpretation of " abs ( H ( s ) ) " as the phase lag.
20.
However, due to the reactance caused by the length difference, the phase lag of the current in the reflector, added to this 180?lag, results in a phase " advance ", and vice versa for the director.
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