Giuliano Tuzzi, Giuseppe Quaranta

DOI Number: N/A

Conference number: IFASD-2017-158

The paper presents the design and optimization of a morphing airfoil, able to change its shape harmonically in a passive way, with the aim of alleviating the loads developed by sinusoidal gust. The study is purely two-dimensional and performed exclusively in the frequency domain, so considering a linear behavior of the aerodynamics. The K ussner and Schwartz frequency domain model is applied to describe the unsteady aerodynamics. An airfoil with the Fishbone architecture has been chosen, as structural system. Such design allows the insertion of pressure chambers in the spine region in order to adaptively modify the chordwise bending stiffness of the structure and to adapt its performances to the frequency of the gust.

Read the full paper here

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.