Parachute fluid-structure interactions: 3-D computation

By Keith Stein, R. Benney, V. Kalro, Tayfun E. Tezduyar, J. Leonard, M. Accorsi. 2000

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A parallel 3D computational method for fluid-structure interactions in parachute systems (2000, methodology): “3D FSI simulations of a round parachute canopy with a flow solver based on the DSD/SST method were reported by Stein et al. [ 12 ].”
Space-time finite element techniques for computation of fluid-structure interactions (2005, methodology): “They are: block-iterative coupling, which we have widely used in our computations (see [19–22]); quasi-direct coupling; and direct coupling.”
Solution techniques for the fully discretized equations in computation of fluid–structure interactions with the space–time formulations (2006, methodology): “They are: block-iterative coupling, which we have widely used in our earlier computations (see [30–33]); quasi-direct coupling [23,24]; and direct coupling [23,24].”
Added-mass effect in the design of partitioned algorithms for fluid-structure problems (2005, methodology): “[21, 20, 17, 5, 4, 11, 12]) Although loosely coupled (explicit) algorithms are successfully used in aeroelasticity (see [5] and the references therein), it is common experience in other applications [19, 10, 16] that they feature instabilities under certain choices of the physical parameters, typica”