AIRCRAFT TRANSONIC FLUTTER CALCULATIONS FOR MULTIPLE-DIRECTION COUPLING VIBRATIONS

来源 :The Second International Symposium on Physics of Fluids(第二届流 | 被引量 : 0次 | 上传用户:bluebird2000
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  Both algebraic method and optimal elliptic partial differential equations are applied to generate multiblock grids.A rapid deforming technique is applied to generate dynamic grids.Finite volume method and dual time-stepping approach is used to solve the unsteady N-S equations, where Spalart-Allmaras One-Equation turbulence model is adopted to the simulations of turbulent flows.A predictor-corrector approach is emploied to solve the structural equations of motion.Then the unsteady N-S equations coupled with structural equations of motion are efficiently solved in the time domain.
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