UVLM

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
Experimental and Numerical Analysis of Unsteady Rotating and Flapping Multi-Wing Systems
matVLM
An UVLM library in MATLAB for multi-body unsteady aerodyanmics.
matVLM
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
PDF Cite Project Slides DOI AIAA SciTech
Numerical and Experimental Investigation of Tandem Wing Flyers
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
PDF Cite Project DOI Aerospace MDPI
Vortex Lattice Simulations of Attached and Separated Flows around Flapping Wings
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
PDF Cite Project DOI AIAA Website
Induced Drag Calculations with the Unsteady Vortex Lattice Method for Cambered Wings
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
PDF Cite Project Slides
Modeling of Aerodynamic Forces in Flapping Flight with the Unsteady Vortex Lattice Method