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Mechanical phenomena in ground run of an aircraft with near-critical slip angles |
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| Authors: | N P Plakhtienko B M Shifrin |
| Institution: | (1) S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, Kiev;(2) State Flight Academy of Ukraine, Kirovograd |
| Abstract: | The paper is concerned with mechanical phenomena accompanying ground run of aircraft with near-critical slip angles. Such phenomena (reduced effectiveness of directional control, self-excited frictional vibrations of a landing gear, internal resonance of an aileron, transverse oscillations of the legs of a multileg landing gear) are due to the nonlinear dependence of the side force on the slip angles __________ Translated from Prikladnaya Mekhanika, Vol. 42, No. 6, pp. 128–135, June 2006. |
| Keywords: | nonlinear dependence side force slip angle mechanical phenomena directional control self-excited frictional oscillations internal resonance aileron transverse vibrations multileg landing gear |
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