TY - JOUR
T1 - An estimate of the second-order in-plane acceleration sensitivity of a Y-cut Quartz thickness-shear resonator
AU - He, Huijing
AU - Yang, Jiashi
AU - Kosinski, John A.
N1 - Publisher Copyright:
© 1986-2012 IEEE.
PY - 2015/8/1
Y1 - 2015/8/1
N2 - We perform a theoretical analysis of the secondorder in-plane acceleration sensitivity of a Y-cut quartz thickness-shear mode resonator. The second-order nonlinear theory of elasticity for anisotropic crystals is used to determine the biasing fields in the resonator under in-plane acceleration. The acceleration-induced frequency shift is determined from a perturbation analysis based on the plate equations for small-amplitude vibrations superposed on a finite bias. We show that, whereas the first-order acceleration-induced frequency shift is zero for a structurally symmetric resonator under in-plane acceleration, the second-order frequency shift is nonzero and is quadratic in the acceleration. As the fourth-order nonlinear elastic constants of quartz have never been measured, we can only estimate the magnitude of the second-order frequency shift. For a particular case of interest, we find Δω/ω0~10-18, 10-16, and 10-14 when the acceleration is 1, 10, and 100 g, respectively.
AB - We perform a theoretical analysis of the secondorder in-plane acceleration sensitivity of a Y-cut quartz thickness-shear mode resonator. The second-order nonlinear theory of elasticity for anisotropic crystals is used to determine the biasing fields in the resonator under in-plane acceleration. The acceleration-induced frequency shift is determined from a perturbation analysis based on the plate equations for small-amplitude vibrations superposed on a finite bias. We show that, whereas the first-order acceleration-induced frequency shift is zero for a structurally symmetric resonator under in-plane acceleration, the second-order frequency shift is nonzero and is quadratic in the acceleration. As the fourth-order nonlinear elastic constants of quartz have never been measured, we can only estimate the magnitude of the second-order frequency shift. For a particular case of interest, we find Δω/ω0~10-18, 10-16, and 10-14 when the acceleration is 1, 10, and 100 g, respectively.
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U2 - 10.1109/TUFFC.2015.007033
DO - 10.1109/TUFFC.2015.007033
M3 - Article
AN - SCOPUS:84939229093
SN - 0885-3010
VL - 62
SP - 1421
EP - 1428
JO - IRE Transactions on Ultrasonic Engineering
JF - IRE Transactions on Ultrasonic Engineering
IS - 8
M1 - 7185009
ER -