Influence of passive deformation in the lift coefficient of a NACA0012 wing model-Reference-Cited by-同舟云学术

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Influence of passive deformation in the lift coefficient of a NACA0012 wing model

Published:2024-05 Issue: Volume:105 Page:338-345
ISSN:0997-7546
Container-title:European Journal of Mechanics - B/Fluids
language:en
Short-container-title:European Journal of Mechanics - B/Fluids

Author:

Duran E.,Lorite-Díez M.,Konovalov-Shishov N.,Gutierrez-Castillo P.,del Pino C.

Funder

Universidad de Málaga

Agencia Estatal de Investigación

Gobierno de España Ministerio de Ciencia e Innovación

Publisher

Elsevier BV

Reference31 articles.

1. C.P. Fagley, J. J. Seidel, T.E. McLaughlin, Aeroelastic Response of a Finite Span NACA 0018 Wing Part 2: Computational Simulations, in: 53rd AIAA Aerospace Sciences Meeting, 2016.

2. Z.Y. Pang, C.E.S. Cesnik, E.M. Atkins., In-Flight Wing Deformation Measurement System for Small Unmanned Aerial Vehicles, in: 55th Structures, Structural Dynamics, and Materials Conference, Vol. 6, 2014, p. 0330.

3. A review on non-linear aeroelasticity of high aspect-ratio wings

4. Correlation analysis of combined and separated effects of wing deformation and support system in the CAE-AVM study

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