PhD Studentship Nonlinear Modelling of Aircraft Gust Loads

PhD Studentship Nonlinear Modelling of Aircraft Gust Loads The project With over 100,000 unsteady aerodynamic simulations required to estimate the maximum loads for each design cycle of a civil aircraft, the introduction of high fidelity analysis into loads prediction is a very challenging and rewarding area of research., The project With over 100,000 unsteady aerodynamic simulations http://www.ischolarshipgrants.com/singapore-scholarship-grants/phd-studentship-nonlinear-modelling-of-aircraft-gust-loads-20130626/,