Fatigue characteristics of stainless steel pin-reinforced composite hat joints

Author:

Ji Hun,Kweon Jin-Hwe,Choi Jin-Ho

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference40 articles.

1. Deo RB, Starns JH, Holzwarth RC. Low-cost composite materials and structures for aircraft application. RTO AVT Specialists’ Meeting. RTO-MP-069(II). London. Norway 2001.

2. Aniversario RB, Harvey ST, McCarty JE, Parson JT, Peterson DC, Pritchett LD, Wilson DR, and Wogulis ER. Full-scale testing, production and cost analysis data for the advanced composite stabilizer for boeing 737 aircraft. NASA Contractor, Report 3649. 1983.

3. Advantages of composite materials in aircraft structures;Muniyasamy;World Acad Sci Eng Technol,2012

4. Mechanics of composite materials;Robert,1999

5. Structural optimization of a hat stiffened panel by response surface techniques;Vitali;J Aircr,2002

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