Efficient Failure Analysis of Laminated Composites and Sandwich Cylindrical Shells Based on Higher-Order Zigzag Theory-Reference-Cited by-同舟云学术

Efficient Failure Analysis of Laminated Composites and Sandwich Cylindrical Shells Based on Higher-Order Zigzag Theory

Author:

Kumar Ajay¹,Chakrabarti Anupam²,Bhargava Pradeep³,Prakash Vipul²

Affiliation:

1. Assistant Professor, Dept. of Civil Engineering, National Institute of Technology Patna, Patna 800005, India (corresponding author).

2. Associate Professor, Dept. of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, India.

3. Professor, Dept. of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

Reference50 articles.

2. Ambartsumyan S. A. (1961). “Theory of anisotropic shells.” Rep. No. 118 National Aeronautics and Space Administration (NASA) Washington DC.

3. A new refined theory of anisotropic shells;Ambartsumyan S. A.;Inst. Math. Mech., Acad. Sci. Arm. SSR, Ere. Transl. Mekh. Polim.,1970

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