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.
Designing vibration strength tests of flight vehicle airborne equipment
Russian Aeronautics (Iz VUZ) ; 52 , 2 ; 145-150
2009-06-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Designing vibration strength tests of flight vehicle airborne equipment
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