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Dynamic ASE Modeling and Optimization of Aircraft with SpaRibs, Phase I

Completed Technology Project

Project Introduction

We propose development and demonstration of a dynamic aeroservoelastic modeling and optimization system based on curvilinear internal structural arrangements of variable topology. This will allow combined sizing and topology optimization of complete airplane configurations including aeroservoelastic performance. More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

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Project Duration

Technology Maturity (TRL)

Technology Areas

A final report document may be available for this project. If you would like to request it, please contact us.