Stochastic Modeling of Preliminary Wing Box Structural Design for Stiffness
Author:
Affiliation:
1. Arizona State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4002
Reference14 articles.
1. Prediction of Wing Structural Mass for Transport Category Aircraft Conceptual Design
2. 3Kallas, D., Brown, K., Ingham, J., Miskin, D. Remsing, T. and Takahashi, T.T., Design of a Dual-Use Aerobatic Light Jet, accepted for publication at the 2018 AIAA Aerospace Sciences Meeting
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1. Structural Analysis and Optimization of Wings Subjected to Dynamic Loads;AIAA Journal;2022-02
2. Design and Validation of Buckling Dominated Wing Structure for Small Unmanned Aerial Systems;AIAA AVIATION 2020 FORUM;2020-06-08
3. Preliminary Design of a Wing Considering Transonic Aerodynamic, Weight and Aeroelastic Behavior;AIAA Aviation 2019 Forum;2019-06-14
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