Abstract
In the framework of designing vibration tests for the airborne equipment units the types of fatigue curves of their elements are determined. A method for recounting the value of the specified unit service life with regard for only vibration effect is proposed. Variants of vibration strength bench tests are considered.
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Original Russian Text © V.G. Zaitsev, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 2, pp. 12–15.
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Zaitsev, V.G. Designing vibration strength tests of flight vehicle airborne equipment. Russ. Aeronaut. 52, 145–150 (2009). https://doi.org/10.3103/S1068799809020032
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DOI: https://doi.org/10.3103/S1068799809020032