Aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV

  • Chen X
  • Han J
N/ACitations
Citations of this article
6Readers
Mendeley users who have this article in their library.

Abstract

For the high-aspect-ratio composite joined-wing UAV, as the geometric nonlinear significant effect, nonlinear aeroelastic analysis method should be applied when study its aeroelastic tailoring method. In the paper, based on the secondary development of MSC/Nastran software with Direct matrix abstraction programme language, with the adopting the multidisciplinary design optimization platform Isight software integrating the MSC/Nastran software analysis, modules of the static aeroelastic analysis, nonlinear static analysis and flutter analysis, a nonlinear aeroelastic tailoring method for high –aspect-ratio composite joined-wing UAV has been presented. Example show that, the method proposed in this paper not only can solve nonlinear aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV problem, but also can be applied to complex engineering structure.

Cite

CITATION STYLE

APA

Chen, X., & Han, J. (2017). Aeroelastic tailoring of high-aspect-ratio composite joined-wing UAV. Mathematical Models in Engineering, 3(1), 41–48. https://doi.org/10.21595/mme.2017.18505

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free