Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings

  • Bach T
  • Hühne C
N/ACitations
Citations of this article
3Readers
Mendeley users who have this article in their library.
Get full text

Cite

CITATION STYLE

APA

Bach, T., & Hühne, C. (2018). Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings. In Advances in Structural and Multidisciplinary Optimization (pp. 838–849). Springer International Publishing. https://doi.org/10.1007/978-3-319-67988-4_64

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