Thomas Lambert
Thomas Lambert
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thesis
Experimental and Numerical Analysis of Unsteady Rotating and Flapping Multi-Wing Systems
PhD thesis in Aerospace Engineering
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Development of numerical models for coaxial rotors (BEMT + UVLM) and tandem flapping wings (UVLM), with experimental validation.
Thomas Lambert
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Project
Optimization of Drone Routing in Humanitarian Applications
Master thesis in General Management
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Quantification of the benefits of using drones to collect information after a disaster.
Thomas Lambert
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Modeling of Aerodynamic Forces in Flapping Flight with the Unsteady Vortex Lattice Method
Master thesis in Aerospace Engineering
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Study and comparison of two approaches used to compute the aerodynamic forces with the UVLM.
Thomas Lambert
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