Characterization of Damage in Triaxial Braided Composites under Tensile Loading-Reference-Cited by-同舟云学术

Characterization of Damage in Triaxial Braided Composites under Tensile Loading

Published:2009-07 Issue:3 Volume:22 Page:270-279
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Littell Justin D.¹²³⁴,Binienda Wieslaw K.¹²³⁴,Roberts Gary D.¹²³⁴,Goldberg Robert K.¹²³⁴

Affiliation:

1. Graduate Student, Univ. of Akron, 302 Buchtel Mall, Akron, OH 44325 (corresponding author).

2. Professor, Univ. of Akron, 302 Buchtel Mall, Akron, OH 44325.

3. Research Materials Engineer, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland OH 44135.

4. Aerospace Engineer, NASA Glenn Research Center, 21000 Brookpark Rd., 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%290893-1321%282009%2922%3A3%28270%29

Reference19 articles.

1. ASTM International. (2006). “Standard test method for tensile properties of polymer matrix composite materials.” ASTM D3039 Philadelphia.

2. Bowman C. L. (2003). “Mechanical properties of triaxial braided carbon/epoxy composites.” Proc. 35th Int. SAMPE Technical Conf.—Materials and Processing: Enabling Flight . . . Our Legacy and Future Dayton Ohio SAMPE Covina Calif.

3. Flexural Testing of Composite Sandwich Structures with Digital Speckle Photogrammetry

4. Investigations of in-plane shear properties of ±45°-carbon/epoxy composites using tensile testing and optical deformation analysis

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