UVLM

µRaptor

An UVLM code for multi-wings flapping, pitching and plunging systems.

µRaptor

Numerical and Experimental Investigation of Tandem Wing Flyers

Conference presentation.
Study of the basic principles governing the aerodynamic properties of tandem wings in close proximity.

Thomas Lambert, N. Warbecq, P. Hendrick, R. Nudds, T. Andrianne, G. Dimitriadis

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

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

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

Modeling of Aerodynamic Forces in Flapping Flight with the Unsteady Vortex Lattice Method