Leclerc, Christophe and Pellegrino, Sergio (2019) Reducing Stress Concentration in the Transition Region of Coilable Ultra-Thin-Shell Booms. In: AIAA Scitech 2019 Forum. AIAA , Reston, VA, Art. No. 2019-1522. ISBN 9781624105784. https://resolver.caltech.edu/CaltechAUTHORS:20190805-134838677
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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.
Item Type: | Book Section | ||||||
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Additional Information: | © 2019 American Institute of Aeronautics and Astronautics. | ||||||
Group: | GALCIT | ||||||
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DOI: | 10.2514/6.2019-1522 | ||||||
Record Number: | CaltechAUTHORS:20190805-134838677 | ||||||
Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20190805-134838677 | ||||||
Official Citation: | Reducing Stress Concentration in the Transition Region of Coilable Ultra-Thin-Shell Booms Christophe Leclerc and Sergio Pellegrino AIAA Scitech 2019 Forum. https://doi.org/10.2514/6.2019-1522 | ||||||
Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||||
ID Code: | 97655 | ||||||
Collection: | CaltechAUTHORS | ||||||
Deposited By: | George Porter | ||||||
Deposited On: | 06 Aug 2019 14:32 | ||||||
Last Modified: | 16 Nov 2021 17:33 |
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