Mechanic-Mathematical Model of Indenting the Rigid Ball Particle into the Indicator Polymer Piezoelectroluminescent Coating

Author:

Pan’kov A. A.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference11 articles.

1. Fegenbaum, Yu.M., Dubinskii, S.V., Bozhevalov, D.G., et al. Obespechenie prochnosti kompozitnykh aviatsionnykh konstruktsii s uchetom sluchainykh ekspluatatsionnykh udarnykh vozdeistvii (Provision of Strength of Composite Aircraft Structures Taking into Account Accidental Operational Impacts), Moscow: Tekhnosfera, 2018.

2. Antuf’ev, B.A., Dynamics of Cylindrical Shell with Locally Damaged Protective Layer, Izv. Vuz. Av. Tekhnika, 2013, vol. 56, no. 3, pp. 7–10 [Russian Aeronautics (Engl. Transl.), 2013, vol. 56, no. 3, pp. 219–223].

3. Gerasimov, A.V. and Pashkov, S.V., Numerical Simulation of Fracture in Thin-Walled Structures by a Group of High-Velocity Elements, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 2, pp. 3–9 [Russian Aeronautics (Engl. Transl.), 2015, vol. 58, no. 2, pp. 137–144].

4. Liang, G., Wang, Y., Mei, D., et al., Flexible Capacitive Tactile Sensor Array with Truncated Pyramids as Dielectric Layer for Three-Axis Force Measurement, J. of Microelectromechanical Systems, 2015, vol. 24. issue 5, pp. 1510–1519.

5. Ramadan, K.S.E., Sameoto, D., and Evoy, S., A Review of Piezoelectric Polymers as Functional Materials for Electromechanical Transducers, Smart Materials and Structures, 2014, vol. 23, article no. 033001.

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