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Shear Stabilization Based Framework for the Failure Testing and Analysis of HSCs

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9453-17-P-0463
Agency Tracking Number: F17A-019-0057
Amount: $149,797.00
Phase: Phase I
Program: STTR
Solicitation Topic Code: AF17A-T019
Solicitation Number: 2017.0
Timeline
Solicitation Year: 2017
Award Year: 2017
Award Start Date (Proposal Award Date): 2017-08-29
Award End Date (Contract End Date): 2018-06-04
Small Business Information
2602 Clover Basin Drive
Longmont, CO 80503
United States
DUNS: 968249636
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Thomas Murphey
 Chief Technologist
 (505) 250-3006
 tom.murphey@roccor.com
Business Contact
 Stephanie Amend
Phone: (720) 515-0527
Email: stephanie.amend@roccor.com
Research Institution
 The University of Colorado
 Dr. Francisco Lopez Jimenez
 (303) 492-1047
 Nonprofit College or University
Abstract

This program will develop an engineering framework for the design and failure analysis of high strain composite (HSC) laminates. The program will first test several HSC laminates to generate a statistically significant dataset for flexural strength. Testing will be performed for short and long term stowage conditions. Initial and ultimate failure modes will be identified and documented using several advanced composite imaging techniques. HSC modeling techniques will be developed using multiscale finite element approaches. These models will include the large and nonlinear hyperelastic deformations needed to model fiber axial nonlinearities and matrix shear nonlinearities. They will also be amenable to time dependent viscoelastic solutions. Using the tools, a shear stabilization based failure criteria for HSCs will be developed. These tools and approaches will allow failure in HSCs to be predicted accurately by including both the effects of laminate stacking sequence and strain gradients in the estimation of compressive failure.

* Information listed above is at the time of submission. *

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