High-velocity impact response of CFRP panels reinforced with stiffeners

Author:

Wang Cunxian,Ren Tengfei,Miao Yinggang,Suo Tao,Tang Zhongbin,Li Yulong

Funder

National Natural Science Foundation of China

111 Project

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference34 articles.

1. Jet engine fan blade containment using an alternate geometry;Carney;Int J Impact Eng,2009

2. High-velocity impact responses of 2618 aluminum plates for engine containment systems under combined actions of projectile form and oblique angle;Wang;Chin J Aeronaut,2019

3. Federal Aviation Administration. Federal aviation regulation part 33, Section 33.94. 1984.

4. Carney KS, Lawrence C, Carney DV. Aircraft engine blade-out dynamics. Seventh international LS-DYNA users conference. Livermore CA, USA: Livermore Software Technology Corporation, 2002:14–26.

5. Experimental and FEM study of thermal cycling induced microcracking in carbon/epoxy triaxial braided composites;Zhang;Compos Part A,2013

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