Abstract
The paper considers the features of the numerical simulation of a thin plate under the thermal shock in the ANSYS package. The temperature fields of one-layer and three-layer plates are investigated. Their comparative analysis is carried out. The features of the results obtained are identified and explained using various models. The presented results can be used to simulate the thermal shock of a thin plate using the ANSYS package.
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References
Boley, B., Weiner, J.: Theory of thermal stresses, p. 580. John Wiley & Sons, New York (1960)
Lykov, A.V.: Application of methods of thermodynamics of irreversible processes to the study of heat and mass transfer. J. Eng. Phys. Thermophys 9(3), 287–304 (1965)
Kartashov, E.M.: Model representations of heat shock in terms of dynamic thermal elasticity. Russian Technol. J. 8(2), 85–108 (2020)
Gadalla, M., Ghommem, M., Bourantas, G., Miller, K.: Modeling and thermal analysis of a moving spacecraft subject to solar radiation effect. Processes 7(11), 807 (2019)
Sedelnikov, A.V., Orlov, D.I.: Development of control algorithms for the orbital motion of a small technological spacecraft with a shadow portion of the orbit. Microgravity Sci. Technol. 32(5), 941–951 (2020)
Shen, Z., Hu, G.: Thermally Induced Dynamics of a Spinning Spacecraft with an Axial Flexible Boom. J. Spacecr. Rocket. 52(5), 1–6 (2015)
Sedelnikov, A.V., Orlov, D.I.: Analysis of the significance of the influence of various components of the disturbance from a temperature shock on the level of microaccelerations in the internal environment of a small spacecraft. Microgravity Sci. Technol. 33(2), 22 (2021)
Belousova, D.A., Serdakova, V.V.: Modeling the temperature shock of elastic elements using a one-dimensional model of thermal conductivity. Int. J. Modeling Simul. Sci. Comput. 11(6), 2050060 (2020)
Sedelnikov, A.V.: The assessment problem of microaccelerations at the experimental sample of the small spacecraft «AIST» after the battery degradation and the method of its solution. Microgravity Sci. Technol. 32(4), 673–679 (2020)
Garmendia, I., Anglada, E., Vallejo, H., Seco, M.: Acurate calculation of conductive conductances in complex geometries for spacecraft thermal models. Adv. Space Res. 57, 1087–1097 (2016)
Sedelnikov, A.V., Rodina, V.S., Orlov, D.I.: Modeling the effect of temperature deformations of large elements on the dynamics of the orbital motion of a small spacecraft. J. Phys: Conf. Ser. 1368, 042074 (2019)
Ivashova, T.A.: The use of measuring current information from solar panels to estimate the angular velocity of rotation of a small spacecraft. In: International Multi-Conference on Industrial Engineering and Modern Technologies (FarEastCon); 2020 Oct 6–9; Vladivostok, Russia, p. 1–6 (2020)
Anshakov, G.P., Belousov, A.I., Sedel’nikov, A.V., Gorozhankina, A.S.: Efficiency estimation of electrothermal thrusters use in the control system of the technological spacecraft motion. Russian Aeronaut. 61(3), 347–354 (2018). https://doi.org/10.3103/S1068799818030054
Chamberlain, M.K., Kiefer, S.H., Banik, J.A.: On-orbit structural dynamics performance of the roll-out solar array. American Institute of Aeronautics and Astronautics Spacecraft Structures Conference 2018. In: Proceedings of the AIAA Spacecraft Structures Conference; 2018 Jan 8–12; Kissimmee. USA. Reston: American Institute of Aeronautics and Astronautics, p. 1–9 (2018)
Sedelnikov, A.V., Filippov, A.S., Gorozhakina, A.S.: Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft. J. Phys: Conf. Ser. 1015, 032045 (2018)
Shen, Z., Tian, Q., Liu, X., Hu, G.: Thermally induced vibrations of flexible beams using Absolute Nodal Coordinate Formulation. Aerosp. Sci. Technol. 29, 386–393 (2013)
Sedelnikov, A.V., Serpukhova, A.A.: Simulation of a flexible spacecraft motion to evaluate microaccelerations. Russian Aeronaut. 52(4), 71–72 (2009)
Tkachenko, S.I., Salmin, V.V., Tkachenko, I.S., Kaurov, I.V., Korovin, M.D.: Verifying parameters of ground data processing for the thermal control system of small spacecraft AIST based on telemetry data obtained by Samara. Proc. Eng. 185, 205–211 (2017)
Sedelnikov, A.V., Potienko, K.I.: Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations. Int. Rev. Aerosp. Eng. 10(3), 160–166 (2017)
Abrashkin, V.I., et al.: Uncontrolled rotary motion of the AIST small spacecraft prototype. Cosm. Res. 55(2), 128–141 (2017)
Sedelnikov, A.V.: Mean of microaccelerations estimate in the small spacecraft internal environment with the use fuzzy sets. Microgravity Sci. Technol. 30(4), 503–509 (2018)
Belousov, A.I., Sedelnikov, A.V.: Probabilistic Estimation of Fulfilling Favorable Conditions to Realize the Gravity-Sensitive Processes Aboard a Space Laboratory. Russian Aeronaut. 56(3), 297–302 (2013)
Orlov, D.I.: Modeling the Temperature Shock Impact on the Movement of a Small Technological Spacecraft. AIP Conf. Proc. 2340, 050001 (2021)
Sedelnikov, A.V.: Algorithm for restoring information of current from solar panels of a small spacecraft prototype «Aist» with help of normality conditions. J. Aeronaut. Astronaut. Aviation 54(1), 67–76 (2022)
Yang, H., Liu, L., Liu, Y., Li, X.: Modeling and micro-vibration control of flexible cable for disturbance-free payload spacecraft. Microgravity Sci. Technol. 33(4), 1–16 (2021). https://doi.org/10.1007/s12217-021-09897-1
Sedelnikov, A.V., Glushkov, S.V., Serdakova, V.V., Evtushenko, M.A., Khnyryova, E.S.: Simulating the stress-strain state of a thin plate after a thermal shock. Int. J. Modeling Simul. Sci. Comput. (2021). https://doi.org/10.1142/S1793962322500246
Taneeva, A.S.: The formation of the target function in the design of a small spacecraft for technological purposes. J. Phys: Conf. Ser. 1901(1), 012026 (2021)
Sedelnikov, A.V., Serdakova, V.V., Khnyryova, E.S.: Construction of the criterion for using a two-dimensional thermal conductivity model to describe the stress-strain state of a thin plate under the thermal shock. Microgravity Sci. Technol. 33(6), 65 (2021)
Acknowledgments
The work was carried out within the framework of the project «Development of scientific and technical foundations and design solutions that ensure the implementation of the required level of microaccelerations on board small spacecraft» (No. 22–19-00483).
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Orlov, D., Serdakova, V., Evtushenko, M., Khnyryova, E., Nikolaeva, A. (2023). Investigating the Features of Various Plate Models Under the Thermal Shock in the ANSYS Package. In: Beskopylny, A., Shamtsyan, M., Artiukh, V. (eds) XV International Scientific Conference “INTERAGROMASH 2022”. INTERAGROMASH 2022. Lecture Notes in Networks and Systems, vol 574. Springer, Cham. https://doi.org/10.1007/978-3-031-21432-5_340
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