RT Conference Proceedings
T1 On the effect of deformation in a wing model on the correlation of the lift slope
A1 Gutiérrez-Castillo, Paloma
A1 Durán-Venegas, Eduardo
A1 Konovalov-Shishov, Nikita
A1 Del-Pino-Peñas, Carlos Manuel
K1 Mecánica de fluidos
AB Deformed wing models with a NACA0012 airfoil are analyzed experimentally in a wind tunnel at theUniversity of Malaga. Measurements show the influence of the level of the deformation on the liftcoefficient and, therefore, on the slope of the lift coefficient versus the angle of attack. In general, thedeformation increments the value of the lift coefficient. This gain is more noticeable for higher windmodels (or higher aspect ratios) and when the wing models are tested at higher Reynolds numbers.We estimated the value of the lift slope with a correlation as a function of Reynolds number andaspect ratio, showing an excellent agreement.
YR 2023
FD 2023
LK https://hdl.handle.net/10630/27369
UL https://hdl.handle.net/10630/27369
LA eng
NO This research has been supported by the project Universidad de Málaga. Campus de Excelencia Internacional Andalucía Tech.PID2021-124692OA-I00 from the Ministerio de Ciencia e Innovación y II Plan Propio UMA
DS RIUMA. Repositorio Institucional de la Universidad de Málaga
RD 21 ene 2026