Residual Property Prediction for Damaged Composite Structures (MSC P 4091)

Award Information
Agency: Department of Defense
Branch: Army
Contract: W31P4Q-13-C-0007
Agency Tracking Number: A122-083-0183
Amount: $149,990.00
Phase: Phase I
Program: SBIR
Awards Year: 2012
Solicitation Year: 2012
Solicitation Topic Code: A12-083
Solicitation Number: 2012.2
Small Business Information
Materials Sciences Corporation
135 Rock Road, Horsham, PA, -
DUNS: 075537910
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Devlin Hayduke
 Engineer
 (215) 542-8400
 hayduke@materials-sciences.com
Business Contact
 Thomas Cassin
Title: President
Phone: (215) 542-8400
Email: cassin@materials-sciences.com
Research Institution
 Stub
Abstract
Advanced composite material systems are vital to the development of lightweight, multi-functional Army missile systems. In addition to reducing the weight of the structure, these material systems provide the ability to expand the function of the structure by tailoring stiffness and strength characteristics for numerous applications. Carbon fiber-reinforced epoxy structures have become very attractive for applications such as solid rocket motor cases, missile airframes, missile guidance housings, as well as many launch tubes and launcher primary structures. The Weapons Development and Integration Directorate within AMRDEC have identified a need to understand the operational fitness of these types of structures following impact events for a wide range of energy levels. The overall objective of the proposed Phase I research program is to develop an analysis tool that allows designers to evaluate post impact residual strength of composite structures. A user element (UEL) subroutine for use with commercially available analysis codes, in particular an improved shell element that offers advantages in both the economy and reliability of computations, is proposed. This novel approach will link the UEL subroutine to a nonlinear material model to evaluate progressive damage of composite materials and a shear correction model that accurately predicts the transverse response of impacted composite structures.

* information listed above is at the time of submission.

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