Thomas Lambert
Thomas Lambert
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Flapping
µRaptor
An UVLM code for multi-wings flapping, pitching and plunging systems.
MechaRaptor
Experimental setup for a medium-size tandem flapping wings system.
Vortex Lattice Simulations of Attached and Separated Flows around Flapping Wings
Journal paper
.
Comparison of three methods for the calculation of loads with the UVLM, applied to flapping wings."
Thomas Lambert
,
N. Abdul Razak
,
G. Dimitriadis
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Project
Project
DOI
Aerospace
Modeling of Aerodynamic Forces in Flapping Flight with the Unsteady Vortex Lattice Method
Master thesis in Aerospace Engineering
.
Study and comparison of two approaches used to compute the aerodynamic forces with the UVLM.
Thomas Lambert
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