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Control of Transition over Aerofoil Surfaces using Active Suction
Linearization techniques
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دروس
FE modelling, modal analysis and model validation of the BRR710 High Pressure Compressor (funded by BMW Rolls-Royce)
Investigation of Alternator Vibration (funded by Robert Bosch GmbH)
A Computational study on robust prediction of transition point over NACA۰۰۱۲ aerofoil surfaces from laminar to turbulent flows
A new CFD method for determination of translational added mass coefficients of an underwater vehicle
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Deep Learning
Biography 40
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