Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection

DOI:10.4121/83e60905-b41f-4460-99a0-376487627108.v1
The DOI displayed above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
DOI: 10.4121/83e60905-b41f-4460-99a0-376487627108

Datacite citation style

Lancelot, Paul; de Breuker, Roeland (2023): Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/83e60905-b41f-4460-99a0-376487627108.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Dataset

This is an aerodynamic reduced order model (ROM) for Matlab/Simulink. It is applied to the scaled-up (x20) OAT15A airfoil, predicting the incremental lift of an arbitrary dynamic aileron deflection at Mach 0.73. The data contains the model and inputs to reproduce Figure 3.10 from the following PhD Dissertation: "Lancelot, P. M. G. J. (2023). Transonic Wing and Control Surface Loads Modelling for Aeroservoelastic Analysis. https://doi.org/10.4233/uuid:e37566e8-cb46-4f90-863d-9cfe0b634507"


History

  • 2023-06-30 first online, published, posted

Publisher

4TU.ResearchData

Format

*.pdf, *.mat, *.igs, *.m, *.png, *.slx

Organizations

TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures and Materials

DATA

Files (9)