aeroelastic deformations efficiency - divergence speed

Version 1.0.1 (3,97 ko) par Tamir Gazit
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow conditions.
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Mise à jour 18 avr. 2020

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Computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different flow conditions, compute the wing’s divergence speed, and investigate the effect of wing sweep on static aeroelasticity. The wing will be modeled as a beam, using finite-elements, and the aerodynamics will be computed via ’Strip Theory’.

User can change the sweep angle, GJ and EI of the wing.
Cl_alpha and Cl_delta

Please feel free to ask questions

Citation pour cette source

Tamir Gazit (2024). aeroelastic deformations efficiency - divergence speed (https://www.mathworks.com/matlabcentral/fileexchange/75087-aeroelastic-deformations-efficiency-divergence-speed), MATLAB Central File Exchange. Récupéré le .

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Créé avec R2020a
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Version Publié le Notes de version
1.0.1

o
1.0.0