Computational Aeroelasticity Using a Pressure-based Solver
Ramji Kamakoti1, Yongsheng Lian1, Sean Regisford1, Andrew Kurdila1, Wei Shyy1
CMES-Computer Modeling in Engineering & Sciences, Vol.3, No.6, pp. 773-790, 2002, DOI:10.3970/cmes.2002.003.773
Abstract The non-linear fluid-structure interaction problem is studied for two different wing configurations based on moving grid techniques. These configurations demonstrate the interaction between a rigid structure and fluid, as well as the interaction between a flexible structure and fluid. A closely-coupled approach is used to perform the combined fluid and structure interaction computations. The flow solver is an unsteady, implicit, three-dimensional, multi-block, pressure-based Navier-Stokes solver. The structure solver for the AGARD wing model is based on a linear, time-invariant model derived via classical structural finite elements whereas the flexible structural solver is based on a More >