Reducing Stress Concentration in the Transition Region of Coilable Ultra-Thin-Shell Booms
- Creators
- Leclerc, Christophe
-
Pellegrino, Sergio
Abstract
High stress concentrations leading to material failure have been observed in TRAC booms coiled under tension around a circular hub. The stress concentrations are typically observed in the transition region between the fully deployed and coiled sections of the boom. A numerical simulation framework is proposed to model the coiling process analyses the stress distribution in the transition region. Isotropic booms are first studied to understand the effects of the cross-section geometry and the boundary conditions during coiling. Compressive stress is reduced by 13% and 26% by using a variable curvature cross-section and adding nip rollers in the coiling mechanism respectively. For an ultra-thin glass fiber-carbon fiber composite laminate, the compressive stress is similarly reduced by 24% and 11%. The variable curvature cross-section is shown to eliminate the stress concentration in the transition region.
Additional Information
© 2019 American Institute of Aeronautics and Astronautics.Additional details
- Eprint ID
- 97655
- Resolver ID
- CaltechAUTHORS:20190805-134838677
- Created
-
2019-08-06Created from EPrint's datestamp field
- Updated
-
2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2019-1522