Thomas Lambert
Thomas Lambert
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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
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