1. Thermoelastic vibration analysis of rotational pre-twisted and curved blades covered with functionally graded thermal barrier coatings.
- Author
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Chen, Yukun, Ye, Tiangui, Jin, Guoyong, Zhong, Saifeng, Lv, Wubin, and Mao, Qizhi
- Subjects
- *
STRAINS & stresses (Mechanics) , *RESIDUAL stresses , *HAMILTON'S principle function , *CORIOLIS force , *ELASTIC plates & shells , *THERMAL stresses - Abstract
• Thermoelastic vibration analysis of rotational pre-twisted FGTBC-coated blades is presented. • CUF combined with 3-D elastic shell theory is used to ensure the calculation accuracy. • A separate deflection analysis is presented to capture initial mechanical-thermal stresses. • An experimental study on vibrations of different pre-twisted shell-type blades is conducted. A quasi-3D theoretical model for analyzing the thermoelastic vibrations of rotational pre-twisted, curved blades coated with functionally graded thermal barrier coatings (FGTBCs) is presented. The FGTBC-coated blades are assumed to operate within a steady-state temperature field. Three temperature distribution models, representing uniform, non-uniform symmetrical, and non-uniform asymmetrical temperature distributions, are derived by solving heat conduction equations established along the blade's thickness direction. The considered blade is theoretically simplified as a twisting shell panel, utilizing the Carrera unified formulation in conjunction with three-dimensional elastic theory to ensure the quasi-3D calculation accuracy. Rotational effects, including the mechanical-thermal prestress stiffening, rotating softening, and Coriolis force, are systematically considered. Accurate mechanical and thermal stress distribution within the FGTBC-coated blade is obtained through a separated quasi-equilibrium static analysis. By incorporating higher-order nonlinear strain terms, the mechanical and thermal prestress stiffening effect is quantified as additional potential energy and involved into the overall energy functional of the system. Thermal-elastic vibration equations of the rotational twisted FGTBC-coated blades are derived using Hamilton's principle. Experimental validations on dynamic modeling of three shell panels with different twisting angles are conducted. The proposed model's convergence and correctness are validated against reported findings, numerical simulations, and experimental test data. Finally, the study analyzes the effects of temperature load, rotation velocity, structural parameters, and material parameters on mechanical-thermal stresses and thermo-elastic vibrations of rotational pre-twisted FGTBC-coated blades. [ABSTRACT FROM AUTHOR]
- Published
- 2025
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