Different causes for structural nonlinearities on aircraft; representation of nonlinear force deflection diagrams of aircraft parts by complex Fourier analysis; approximate method for solution of nonlinear flutter equations is developed using systems of homogeneous linear equations; special case of harmonic balance is compared with more accurate solutions. (Received Sept 1960)
On nonlinear approach to aeroelastic stability theory
AGARD -- Report
AGARD -- Reports ; n 246
1959
17 pages
Report
English
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Rotorcraft Aeroelastic Stability
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