Coupled Analysis of Low-Velocity Impact Damage and Compression after Impact Strength of Composite Laminates-Reference-Cited by-同舟云学术

Coupled Analysis of Low-Velocity Impact Damage and Compression after Impact Strength of Composite Laminates

Published:2021-09 Issue:5 Volume:34 Page:04021051
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Borkowski Luke B.¹,Kumar Rajesh S.²^ORCID,Palliyaguru Upul R.³

Affiliation:

1. Staff Research Engineer, Raytheon Technologies Research Center, 411 Silver Lane, East Hartford, CT 06118.

2. Associate Director-Research, Raytheon Technologies Research Center, 411 Silver Lane, East Hartford, CT 06118 (corresponding author). ORCID: .

3. Senior Research Engineer, National Institute for Aviation Research, Wichita State Univ., 1845 Fairmount St., Wichita, KS 67260.

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.1943-5525.0001281

Reference51 articles.

1. On the relationship between failure mechanism and compression after impact (CAI) strength in composites

2. Abrate, S. 2005. Impact on composite structures. Cambridge, UK: Cambridge University Press.

3. Aoki Y. H. Samejima H. Suemasu and Y. Nagao. 2009. “Effect of thickness on impact damage and CAI behavior.” In Proc. ICCM-17 17th Int. Conf. on Composite Materials. Edinburgh UK: International Conference on Composite Materials.

4. Inverse method for estimation of composite kink-band toughness from open-hole compression strength data

5. Mechanics-Based Model for Rapid Prediction of Low-Velocity Impact Damage in Composite Laminates

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