2016 13th International Scientific-Technical Conference on Actual Problems of Electronics Instrument Engineering (APEIE) 2016
DOI: 10.1109/apeie.2016.7806427
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Methods of providing reliability of avionics and aerospace equipment at the design stage

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Cited by 9 publications
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“…The rod length is l = 1500 mm. The second natural frequency of the longitudinal oscillations (according to formula [3]) is f2 = 3459 Hz (taken as an example). The right edge of the rod is driven at this frequency through the fastening; the harmonic wave will propagate along the rod with the same speed as in the rod with free ends.…”
Section: Computational Experimentsmentioning
confidence: 99%
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“…The rod length is l = 1500 mm. The second natural frequency of the longitudinal oscillations (according to formula [3]) is f2 = 3459 Hz (taken as an example). The right edge of the rod is driven at this frequency through the fastening; the harmonic wave will propagate along the rod with the same speed as in the rod with free ends.…”
Section: Computational Experimentsmentioning
confidence: 99%
“…According to analytical formula [3], the first four natural fluctuation frequencies of the rod fixed at the ends of l = 1500 mm length, are identified: f1 = 1729 Hz, f2 = 3459 Hz, f3 = 5188 Hz, f4 = 6198 Hz.…”
Section: Computational Experimentsmentioning
confidence: 99%
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