Kevin McHugh, Cate Leszcz, Joshua Deaton

DOI Number: N/A

Conference number: IFASD-2024-002

This work investigates a new method to design aircraft skin panels to minimize weight while providing sufficient strength to withstand both buckling due to aerodynamic heating and flutter due to dynamic pressure over the panel. In this work, mass minimization is done via an optimization of panel thickness distribution as opposed to fill-void techniques or methods of adding discrete stiffeners found in the literature or in practice. The thickness distribution and therefore optimization problem is further reduced in numerical order by utilizing a Galerkin projection of global thickness basis functions. The developed tool results in a 6-17% reduction in weight for an optimized panel for thermal buckling stability when compared to the optimally thin flat panel.

Read the full paper here

In Categories: 1. IFASD 2024, 1.Events, Computational Aeroelasticity
Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.