Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings

TR Number

Date

2017-09-19

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Virginia Tech

Abstract

Description

Keywords

SpaRibs, bilevel programming optimization, aeroelastic tailoring, active aeroelastic wing, curvilinearly stiffened composite panel

Citation

Persistent link

http://hdl.handle.net/10919/79143

Collections

Doctoral Dissertations

We collect and process your personal information for the following purposes: Authentication, Preferences, Acknowledgement and Statistics.
To learn more, please read our privacy policy.

Customize