A Novel Composite Design Optimization Method for Minimized Manufacturing Cost with Improved Performances
Author:
Publisher
Springer Science and Business Media LLC
Subject
Ceramics and Composites
Link
https://link.springer.com/content/pdf/10.1007/s10443-022-10027-2.pdf
Reference50 articles.
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2. Silva, G.H.C., Do Prado, A.P., Cabral, P.H., De Breuker, R., Dillinger, J.K.S.: Tailoring of a composite regional jet wing using the slice and swap method. J. Aircr. 56, 990–1004 (2019). https://doi.org/10.2514/1.C035094
3. Rajpal, D., Mitrotta, F.M.A., Socci, C.A., Sodja, J., Kassapoglou, C., De Breuker, R.: Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance. Compos. Struct. 275, 114373 (2021). https://doi.org/10.1016/j.compstruct.2021.114373
4. Townsend, S., Kambampati, S., Kim, H.A.: Aeroelastic optimization of wing skin using a level set method. 2018 Multidiscip. Anal. Optim. Conf. (2018). https://doi.org/10.2514/6.2018-3878
5. Chiozzotto, G.P.: Initial weight estimate of advanced transport aircraft concepts considering aeroelastic effects. AIAA SciTech Forum - 55th AIAA Aerosp. Sci. Meet. (2017). https://doi.org/10.2514/6.2017-0009
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