Transactions of Nanjing University of Aeronautics & Astronautics
Archive > Volume 35 Issue 1 > 2018,35(1):109-115. DOI:10.16356/j.1005-1120.2018.01.109 Prev Next

Vibration analysis, control and utilization

Double Peak Derived from Piezoelectric Coefficient Nonlinearity and Proposal for Self-Powered Systems

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