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A powerful model to predict aeroacoustic interactions in the linear regime is the perturbed compressible linearized Navier Stokes equations.
This work advances the development of nanowire resonators that are working beyond linear regime.
The linear regime, where G' and G″ are constant regardless of strain amplitude, is clearly observed.
Such a linear regime could be explained by two mechanisms, either the PAT or the PASRH.
Furthermore, the spin split of band z0 leads to the spin polarization in the linear regime.
The linear regime of the transfer characteristics was used to obtain the slope ΔId/ΔVg.
Friction results at all applied loads show linear regime of friction.
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In a non-linear regime, it can become unwieldy and unreliable.
At room-temperature, a clear transition is observed at 20 pA between a linear and a non-linear regime.
When the absorption strength is enhanced, the emission increases with the square of the enhancement in the non-linear regime.
These numerical simulations illustrate the capabilities of the FE2 strategy under non-linear regime.
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