aeroelastic deformations efficiency - divergence speed
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow conditions.
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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
Cite As
Tamir Gazit (2026). aeroelastic deformations efficiency - divergence speed (https://uk.mathworks.com/matlabcentral/fileexchange/75087-aeroelastic-deformations-efficiency-divergence-speed), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.0.1 (3.97 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
