Agile Wing Integration - Nonlinear devices on a strut for loads control

Project Details

Description

The Commercial Air Transport Industry is about to undergo a step-change to meet future economic, mobility and environmental challenges. This proposal was submitted as part of a wider set of Overall Aircraft Design projects under the Airbus Wing of the Future Research Programme and it aimed to position Airbus and its partners at the forefront of this change by developing rapid, world-beating Wing Design and Integration capability and solutions for use during the early phases of an aircraft product development cycle. The project aimed to achieve this by building on the 4 themes of: Conceptual Definition, Design and Integration, Demonstration/Validation, Learning

Layman's description

Work Package 2.2.3: Nonlinear devices on a strut for loads control

Key findings

This research is summarized in the dissertation written by Dr Szczyglowski.
Alternative titleWork Package 2.2.3: Nonlinear devices on a strut for loads control
AcronymAWI
StatusFinished
Effective start/end date1/04/1430/09/18

Structured keywords

  • AWI

Fingerprint

Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.