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
引用格式
Tamir Gazit (2024). aeroelastic deformations efficiency - divergence speed (https://www.mathworks.com/matlabcentral/fileexchange/75087-aeroelastic-deformations-efficiency-divergence-speed), MATLAB Central File Exchange. 检索来源 .
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