Development of an Orthotropic Elasto-Plastic Generalized Composite Material Model Suitable for Impact Problems-Reference-Cited by-同舟云学术

Development of an Orthotropic Elasto-Plastic Generalized Composite Material Model Suitable for Impact Problems

Published:2016-07 Issue:4 Volume:29 Page:04015083
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Goldberg Robert K.¹,Carney Kelly S.²,DuBois Paul³,Hoffarth Canio⁴,Harrington Joseph⁵,Rajan Subramaniam⁶,Blankenhorn Gunther⁷

Affiliation:

1. Aerospace Engineer, Structures and Materials Division, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135 (corresponding author).

2. Aerospace Engineer, Structures and Materials Division, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135.

3. Research Scientist, George Mason Univ., 4400 University Dr., Fairfax, VA 22030.

4. Ph.D. Student, School of Sustainable Engineering, Arizona State Univ., 1151 S. Forest Ave., Tempe, AZ 85287.

5. School of Sustainable Engineering, Arizona State Univ., 1151 S. Forest Ave., Tempe, AZ 85287.

6. Professor, School of Sustainable Engineering, Arizona State Univ., 1151 S. Forest Ave., Tempe, AZ 85287.

7. Software Engineer, Livermore Software Technology Corporation, 7374 Los Positas Rd., Livermore, CA 94551.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000580

Reference21 articles.

1. Bednarcyk B. A. and Arnold S. M. (2002). “MAC/GMC 4.0 user’s manual–Keywords manual.” NASA/TM-2002-212077/VOL2 National Aeronautics and Space Administration Washington DC.

2. Bogert P. B. Satyanarayana A. and Chunchu P. B. (2006). “Comparison of damage path predictions for composite laminates by explicit and standard finite element analysis tools.” 47th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. American Institute for Aeronautics and Astronautics Washington DC.

3. A Progressive Damage Model for Laminated Composites Containing Stress Concentrations

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