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Modeling of landing of a helicopter with skid undercarriage with regard for the second landing impact
Authors:S A Mikhailov  L V Korotkov  S A Alimov  D V Nedel’ko
Institution:1.Tupolev Kazan National Research Technical University,Kazan,Russia;2.OAO Kazan Helicopters,Kazan,Russia
Abstract:A technique is suggested for calculating the helicopter spatial motion and the stress-strain state of a skid landing gear in the course of landing with regard for the second landing impact; geometric, material and design nonlinearity of undercarriage springs deformation is taken into account. The comparison between the analysis results and experimental data is presented.
Keywords:
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