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For many years, compared with conventional aircraft, helicopters were underpowered, difficult to control, and subject to much higher dynamic stresses that caused material and equipment failures.
However, their response to dynamic stresses is poorly defined.
We see in Fig. 5, large values of accelerations at startup, which means high dynamic stresses.
The dynamic stresses in the triggered regions range from several kPa to tens of kPa.
The operation of the machine may introduce severe dynamic stresses on the beam.
These collisions create local dynamic stresses against which the structural elements should be designed for.
This is the principle of the rockburst induced by static and dynamic stresses superposition, as shown in Fig. 1.
One of challenging issues in structural random analysis is to accurately predict the dynamic stresses.
The operation of machine may introduce severe dynamic stresses on the beam.
The loss factor is also influenced by the frequency and magnitude of local dynamic stresses.
It is shown that the second mechanism can cause dangerously large dynamic stresses in the riser.
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