Flexible aircraft dynamics with a geometrically-nonlinear description of the unsteady aerodynamics
The Unsteady Vortex-Lattice Method provides a medium-fidelity tool for the prediction of non-stationary aerodynamic loads in low-speed, but high-Reynolds-number, attached flow. Despite a proven track record in applications where free-wake modelling is critical, other models based on potential-flow t...
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Imperial College London
2012
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| Online Access: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.556602 |