Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach-Reference-Cited by-同舟云学术

Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach

Published:2015-09 Issue:5 Volume:28 Page:04014117
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cater Christopher R.¹,Xiao Xinran²,Goldberg Robert K.³,Kohlman Lee. W.³

Affiliation:

1. Graduate Research Assistant, Mechanical Engineering, Michigan State Univ., Composite Vehicle Research Center, Lansing, MI 28910 (corresponding author).

2. Associate Professor, Mechanical Engineering, Michigan State Univ., Composite Vehicle Research Center, Lansing, MI 28910.

3. Research Aerospace Engineer, NASA Glenn Research Center, Cleveland, OH 44135.

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.1943-5525.0000445

Reference42 articles.

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2. Blinzler B. J. (2012). “Systematic approach to simulating impact for triaxially braided composites.” Ph.D. thesis Univ. of Akron Akron OH.

3. Branch K. Shivakumar K. and Awa V. S. (1996). “Three-dimensional tow inclination model for calculating elastic constants of three-dimensional triaxial braided composites.” AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA 1788–1803.

4. Longitudinal Elastic Modulus Prediction of a 2-D Braided Fiber Composite

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