Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials

Award Information
Agency:
Department of Defense
Amount:
$99,719.00
Program:
STTR
Contract:
FA9550-09-C-0096
Solitcitation Year:
2008
Solicitation Number:
2008.A
Branch:
Air Force
Award Year:
2009
Phase:
Phase I
Agency Tracking Number:
F08A-025-0133
Solicitation Topic Code:
AF08-T025
Small Business Information
COMET TECHNOLOGY CORP.
3830 Packard, Suite 110, Ann Arbor, MI, 48108
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
Y
Duns:
136770703
Principal Investigator
 Satha Raveendra
 President
 (734) 973-1600
 rraveendra@cometacoustics.com
Business Contact
 Satha Raveendra
Title: President
Phone: (734) 973-1600
Email: rraveendra@cometacoustics.com
Research Institution
 UNIV. OF MICHIGAN
 Krista L Campeau
 3003 South State Street
Ann Arbor, MI, 48109 1274
 (734) 936-1289
 Nonprofit college or university
Abstract
This proposal is concerned with the development of a novel failure initiation and progressive failure analysis (PFA) modeling method for advanced composite structures. The laminate is modeled as a collection of degrading lamina within the framework of lamination theory and executed using user defined subroutines through a commercial finite element software package. In the proposed approach, designated as “progressive failure analysis tool”, (PFAT), computations will be simultaneously carried out in parallel at three length scales, as needed (the laminate level (LAM), the lamina level (LL) and at the level of a fiber/matrix (FM) unit cell representation of the lamina), with strong coupling between the three scales. The results to be obtained will provide the necessary guidance in selecting the most robust methodology to achieve the desired goal of combining initial design with reliability based tools to re-design a composite structure. The proposal utilizes a fundamental physics based approach that is devoid of empirical formulas that have dominated failure prediction tools in composites.

* information listed above is at the time of submission.

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