KiranRamesh-Aero / UnsteadyFlowSolvers.jl

Solvers for problems involving unsteady fluid flow
MIT License
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Added two trailing-edge separation experimental solvers #16

Open mszudarek opened 7 years ago

mszudarek commented 7 years ago

ldvm_klb_tr solver for unsteady separated flows; Leishman-Beddoes dynamic stall model formulas for forces are used to account for flow separation.

ldvm_spv solver for unsteady separated flows; vortices are shed from separation point location. Only NACA 00XX aerofoils supported, no LEV supported.

Notebooks explaining and validating the code are present.