Aerospace Engineering > GATE 2014 > Aircraft Stability
In most airplanes, the Dutch roll mode can be excited by applying
Correct : b
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Consider the following four statements regarding aircraft longitudinal stability:P. CM,cg at zero lift must be positiveQ. ∂CM,cg/∂aa must be negative...
Consider the following four statements regarding aircraft longitudinal stability:P. CM,cg at zero lift must be positiveQ. ∂CM,cg/∂aa must be negative...
Consider the following four statements regarding aircraft longitudinal stability:P. CM,cg at zero lift must be positiveQ. ∂CM,cg/∂aa must be negative...
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