System and Method for Dynamic Aeroelastic Control

TBMG-25698

11/01/2016

Abstract
Content

Innovators at NASA’s Armstrong Flight Research Center are developing a collection of algorithms that can accurately determine the structural state of an aircraft. This work is in response to new airframe designs that save weight — and thereby improve fuel efficiency — by removing stiffness in the wings and incorporating lighter materials such as composites.

Meta TagsDetails
Citation
"System and Method for Dynamic Aeroelastic Control," Mobility Engineering, November 1, 2016.
Additional Details
Publisher
Published
Nov 1, 2016
Product Code
TBMG-25698
Content Type
Magazine Article
Language
English