Thomas Lambert
Thomas Lambert
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Experimental and Numerical Analysis of Unsteady Rotating and Flapping Multi-Wing Systems
PhD thesis in Aerospace Engineering
.
Development of numerical models for coaxial rotors (BEMT + UVLM) and tandem flapping wings (UVLM), with experimental validation.
Thomas Lambert
Project
Project
Project
Rotare
A feature-rich and Open-Source implementation of the BEMT in Matlab
MechaRaptor
Experimental setup for a medium-size tandem flapping system.
matVLM
An UVLM library in MATLAB for multi-body unsteady aerodyanmics.
Experimental Analysis of a Large-scale Tandem Flapping Wing System
Conference presentation
.
Experimental measurements on a medium scale prototype of tandem flapping wings system.
Thomas Lambert
,
G. Dimitriadis
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DOI
AIAA
SciTech
Numerical and Experimental Investigation of Tandem Wing Flyers
Conference presentation
.
Analysis of the basic principles governing the aerodynamic behavior of tandem wings in close proximity.
Thomas Lambert
,
N. Warbecq
,
P. Hendrick
,
R. Nudds
,
T. Andrianne
,
G. Dimitriadis
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Project
Slides
DOI
AIAA
SciTech
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
DOI
Aerospace MDPI
Induced Drag Calculations with the Unsteady Vortex Lattice Method for Cambered Wings
Journal paper
.
Comparison of two approaches for the load calculation with the UVLM, applied to cambered wings.
Thomas Lambert
,
G. Dimitriadis
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Project
DOI
AIAA Website
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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