Optimization of blended bistable laminate for morphing flap

Ajit S. Panesar, Paul M. Weaver

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Multistable composite structures offer a potential platform for the development of morphing flight vehicles. The recent advance in tow-placement technology has enabled the blending of multistable sections with major structural components thereby enhancing the overall structural performance of the flight vehicle. The use of ant colony systems as an optimization concept has been implemented by incorporating the feedback from the finite element analysis on a blended bistable laminate for a morphing flap application.

Original languageEnglish
Title of host publication51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Publication statusPublished - 2010
Externally publishedYes
Event51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Orlando, FL, United States
Duration: 12 Apr 201015 Apr 2010

Publication series

NameCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
ISSN (Print)0273-4508

Conference

Conference51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Country/TerritoryUnited States
CityOrlando, FL
Period12/04/1015/04/10

Fingerprint

Dive into the research topics of 'Optimization of blended bistable laminate for morphing flap'. Together they form a unique fingerprint.

Cite this