University of Surrey

Test tubes in the lab Research in the ATI Dance Research

Optimization of the Natural Frequency and Buckling Analysis of Bistable Carbon Fiber Reinforced Plastic Booms for Space Applications

Wu, C, Viquerat, AD and Aglietti, G (2016) Optimization of the Natural Frequency and Buckling Analysis of Bistable Carbon Fiber Reinforced Plastic Booms for Space Applications In: 3rd AIAA Spacecraft Structures Conference, 2016-01-04 - 2016-01-08, San Diego, CA.

[img]
Preview
PDF (licence)
SRI_deposit_agreement.pdf
Available under License : See the attached licence file.

Download (33kB) | Preview

Abstract

Bistable composite shells patented as Bistable Reeled Composite (BRC) booms have the potential to be used as lightweight structural elements for a number of space applications. This paper details an approach to increase the natural frequency and stiffness of BRCs. The motivation for this research is the desire to increase the scalability of a flexible "roll-up" solar array which, in its deployed state, consists of two cantilevered BRCs supporting a flexible Photo Voltaic (PV) cell covered blanket between them. A Finite Element (FE) numerical model is combined with a nonlinear constrained optimization to maximize the natural frequency of BRC booms with respect to the fiber orientation angles and ply discontinuity locations. The results demonstrate that careful selection of the fiber orientation angles and the location of step thickness variations can significantly optimize the natural frequency. Experimental verification of the vibration characteristics of optimized BRC booms has also been conducted. Finally, stability analysis of the optimized BRC booms under bending has been carried out using FE simulation to quantify the Maximum Rotational Acceleration (MRA) that they can take before failure.

Item Type: Conference or Workshop Item (Conference Paper)
Subjects : Surrey Space Centre
Divisions : Faculty of Engineering and Physical Sciences > Electronic Engineering > Surrey Space Centre
Authors :
AuthorsEmailORCID
Wu, CUNSPECIFIEDUNSPECIFIED
Viquerat, ADUNSPECIFIEDUNSPECIFIED
Aglietti, GUNSPECIFIEDUNSPECIFIED
Date : 6 January 2016
Identification Number : 10.2514/6.2016-1472
Copyright Disclaimer : Copyright 2016 American Institute of Aeronautics and Astronautics
Related URLs :
Additional Information : Full text not available from this repository.
Depositing User : Symplectic Elements
Date Deposited : 19 Aug 2016 15:42
Last Modified : 19 Aug 2016 15:42
URI: http://epubs.surrey.ac.uk/id/eprint/811746

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year


Information about this web site

© The University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom.
+44 (0)1483 300800