Experimental development of a constitutive model for high-speed impact containment fabrics

Earth and Space Conference 2008: Proceedings of the 11th Aerospace Division International Conference on Engineering, Science, Construction, and Operations in Challenging Environments

Volumn 323, Issue , 2008, Pages

  Zhu, D ^a   Bansal, S ^a   Naik, D ^a   Mobasher, B ^a   Rajan, S D ^a   Pereira, M ^b  

^a Arizona State University   (United States)

^b NASA GRC   (United States)

Author keywords

Constitutive modeling; Engine fan blade out containment; Explicit finite element analysis; Fabrics; Kevlar; Strain rate effects

Indexed keywords

CONSTITUTIVE MODELS; EARTH (PLANET); FABRICS; FRICTION; NASA; PROJECTILES; STRAIN RATE; TENSILE TESTING;

COEFFICIENT OF FRICTIONS; EXPERIMENTAL DEVELOPMENT; EXPLICIT FINITE ELEMENT ANALYSIS; FAN BLADES; FINITE ELEMENT METHODOLOGY; HIGH-SPEED PROJECTILES; KEVLAR; STRAIN RATE EFFECT;

FINITE ELEMENT METHOD;

EID: 70349386588     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1061/40988(323)87     Document Type: Conference Paper

References (10)

1. ASTM-D-3039, Standard Test Method for Tensile Properties of Fiber-Resin Composites, 2000.
2. Dupont, Kevlar, Retrieved from http://www.dupont.com/kevlar, 2003.
3. Gomuc, Reha, "Explicit Finite Element Analysis of Multi-Layer Composite Fabric for Gas Turbine Engines Containment System: Tasks 3 and 4", FAA Final Report, 2003.
4. Rajan S. D., Mobasher, B., Sharda, J., Yanna, V., Deenadaylu, C., Lau, D. and Shah, D. "Explicit Finite Element Analysis Modeling of Multi-Layer Composite Fabric for Gas Turbine Engines Containment Systems Part 1- Static Tests amd Modeling,", Final report, DOT/FAA/AR-04/40,P1 Office of Aviation Research, Wash., D.C. 20591, Nov. 2004.
5. Sharda, J., "Mechanical Testing & Finite Element Analysis of Fabrics for Engine Containment Systems", M.S. Thesis, Department of Civil & Environmental Engineering, Arizona State University, 2002.
6. Tabiei, A. and Jiang, Y., "Woven fabric composite material model with material nonlinearity for nonlinear finite element simulation", International Journal of Solids and Structures, 36, 2757-2771, 1999.
7. Toyobo, Zylon, http://www.toyobo.co.jp/e/seihin/kc/pbo/menu/fra-menu-en. htm, 2003.
8. Pereira, J.M. and Revilock, D.M. (2004). "Explicit Finite Element Modeling of Multilayer Composite Fabric for Gas Turbine Engine Containment Systems. Part 2: Ballistic Impact Testing", DOT/FAA/AR-04/40,P2.
9. Sharda, J., Deenadayalu, C., Mobasher, B. and Rajan, S. D. (2006). "Modeling of Multi-Layer Composite Fabrics for Gas Turbine Engine Containment Systems", ASCE J of Aerospace Engineering, 19:1, 38-45.
10. Stahlecker, Z., Mobasher, B., Rajan, S.D. and Pereira, M. (2008). "Development of Reliable Modeling Methodologies for Engine Fan Blade Out Containment Analysis. Part II: Finite Element Analysis", International Journal of Impact Engineering, submitted for Publication.