Self-oscillations of aircraft landing gear shock-strut at considerable non-linear friction
<p><em> The report considers self-oscillations at ε >1. The previous works were dedicated to the elastic frictional L.G. shock strut oscillations, the mathematical model of which is a non-linear differential equation with low ε parameter of its right-hand part.</em></p>...
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| Format: | Article |
| Language: | English |
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National Aviation University
2004-01-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/989 |