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Showing 1 to 1 of 1 for “"flexibles Flugzeug"”.
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Approximative Stabilitätsanalyse der nichtlinearen Dynamik von Flugzeugen
A method for the nonlinear analysis of dynamic systems and its application to aircraft is presented. In extension of existing averaging methods this procedure follows the linearizing eigenvalue analysis, but defines the eigenvalue and eigenvector as functions of the deflection from the examined …