aeroelastic deformations efficiency - divergence speed

Versión 1.0.1 (3,97 KB) por Tamir Gazit
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow conditions.
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Actualizado 18 abr 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

Citar como

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

Compatibilidad con la versión de MATLAB
Se creó con R2020a
Compatible con cualquier versión
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Más información sobre Aerodynamics en Help Center y MATLAB Answers.

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Versión Publicado Notas de la versión
1.0.1

o

1.0.0