On computing dynamic loads on flight control surfaces subjected to impact
2018 ◽
pp. 51-58
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Predicting structure properties at the initial design stage is especially important for products that will undergo vibration and impact when used. The paper presents a technique for computing dynamic loads on an aircraft rudder arm when it strikes an arrester as it unfolds in flight. We used a finite element software package to analyse the natural vibrations of the structure.
2015 ◽
Vol 802
◽
pp. 208-213
1995 ◽
2009 ◽
Vol 419-420
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pp. 673-676
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2012 ◽
Vol 518-523
◽
pp. 1720-1723
1996 ◽
Vol 11
(3)
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pp. 331-341
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