Numerical Simulation of an A320 Morphing Wing Through Frequency Modulation in the Vicinity of the Trailing Edge in Subsonic Regimes
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-61109-4_12
Reference27 articles.
1. Chinaud M, Rouchon JF, Duhayon E, Scheller J, Cazin S, Marchal M, Braza M (2014) Trailing-edge dynamics and morphing of a deformable flat plate at high Reynolds number by time-resolved PIV. J Fluids Struct 47:41–54. https://doi.org/10.1016/j.jfluidstructs.2014.02.007
2. Scheller J, Chinaud M, Rouchon JF, Duhayon E, Cazin S, Marchal M, Braza M (2015) Trailing-edge dynamics of a morphing NACA0012 aileron at high Reynolds number by high-speed PIV. J Fluids Struct 55:42–51. https://doi.org/10.1016/j.jfluidstructs.2014.12.012
3. Jodin G, Motta V, Scheller J, Duhayon E, Döll C, Rouchon JF, Braza M (2017) Dynamics of a hybrid morphing wing with active open loop vibrating trailing edge by time-resolved PIV and force measures. J Fluids Struct 74:263–290. https://doi.org/10.1016/j.jfluidstructs.2017.06.015
4. Jodin G, Scheller J, Duhayon E, Rouchon JF, Braza M (2017) Implementation of a hybrid electro-active actuated morphing wing in wind tunnel. Solid State Phenomena, Trans Tech Publications 2017, vol 260, pp 85–91. https://doi.org/10.4028/www.scientific.net/SSP.260.85
5. Scheller J (2015) Electroactive morphing for the aerodynamic performance improvement of next generation airvehicles. PhD Thesis, Toulouse INPT-IMFT. https://oatao.univ-toulouse.fr/14479/
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