An Optimal Trim Configuration Optimization Framework for Highly Flexible Aircraft
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-3998-1_86
Reference8 articles.
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2. Nguyen, N., Trinh, K., Reynolds, K., Kless, J., Aftosmis, M., Urnes, J.: Elastically shaped wing optimization and aircraft concept for improved cruise efficiency. In: 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Grapevine (Dallas/Ft. Worth Region). American Institute of Aeronautics and Astronautics, Texas (2013). https://doi.org/10.2514/6.2013-141
3. Molinari, G., Arrieta, A.F., Guillaume, M., Ermanni, P.: Aerostructural performance of distributed compliance morphing wings: wind tunnel and flight testing. AIAA J. 54(12), 3859–3871 (2016). https://doi.org/10.2514/1.J055073
4. Hammerton, J.R., Weihua, S., Zhu, G., Swei, S.-M.: Optimum distributed wing shaping and control loads for highly flexible aircraft. Aerosp. Sci. Technol. 79, 255–265 (2018). https://doi.org/10.1016/j.ast.2018.05.045
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