Computation of Viscous Phenomena in Unsteady Transonic Flow,
DEUTSCHE AIRBUS G M B H BREMEN (GERMANY F R)
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Progress in the development towards a 30 viscous-inviscid strong interaction method for computing unsteady transonic wing flow is reported. In the current version, an ADI-technique for solving the 3D unsteady Transonic Small Perturbation Equation TSP has been extended by incorporating an unsteady 2D integral boundary layer method and then simultaneously solving the viscous and inviscid flow equations in a stripwise fashion.
- Fluid Mechanics