Chinese Journal of Aeronautics · 2014 · 38 citations · 18 references
EngineeringComputational EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsAerodynamic DesignComputational AerodynamicsComputational Fluid-structure InteractionDragNumerical Drag SimulationNumerical ModelingNumerical Wind TunnelOperator SplittingWind Tunnel ModelingWind Tunnel Simulation
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shaped folded parachute with detailed structures is established. The simplified arbitrary Lagrangian–Eulerian fluid–structure interaction (SALE/FSI) method is used to simulate the inflation process of a folded parachute, and the flow field calculation is mainly based on operator splitting technique. By using this method, the dynamic variations of related parameters such as flow field and structure are obtained, and the load jump appearing at the end of initial inflation stage is captured. Numerical results including opening load, drag characteristics, swinging angle, etc. are well consistent with wind tunnel tests. In addition, this coupled method can get more space–time detailed information such as geometry shape, structure, motion, and flow field. Compared with previous inflation time method, this method is a completely theoretical analysis approach without relying on empirical coefficients, which can provide a reference for material selection, performance optimization during parachute design.
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Tayfun E. Tezduyar, Marek Behr, J. Liou · Computer Methods in Applied Mechanics and Engineering · 1992 · 832 citations
Computing, Computational Engineering, Mechanical Engineering +11
Tayfun E. Tezduyar, Marek Behr, Sanjay Mittal et al. · Computer Methods in Applied Mechanics and Engineering · 1992 · 677 citations
Engineering, Computational Engineering, Mechanical Engineering +17