Research of vibratory loads on power units parts and assemblies under design, test and ground development of aircraft constructions

The article describes the scientific and methodological aspects of analysis of processes in highpower units, which at the stage of design and analysis of their kinematic and dynamic characteristics, during tests and ground tests of aircraft structures permit to rule out an increased level of vibration during operation of the units in a wide speed range, excluding the occurrence of resonance phenomena and the destruction of their structural elements in service.

References

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