Challenges in Processing of a Cocured Wing Test Box Using Vacuum Enhanced Resin Infusion Technology (VERITy)

Procedia Materials Science - Tập 6 - Trang 331-340 - 2014
Kundan Kumar Verma1, B.L. Dinesh1, Kailash Singh1, Kotresh M. Gaddikeri1, Ramesh Sundaram1
1Advanced Composites Division, CSIR-National Aerospace Laboratories, Bengaluru – 560017, India

Tài liệu tham khảo

Boh, 2005, Damage modeling of SCRIMP woven roving laminated beams subjected to transverse shear, Composites B, 36, 427, 10.1016/j.compositesb.2005.01.001 Correia, 2004, Use of Resin Transfer Moulding Simulation to Predict Flow, Saturation and Compaction in the VARTM Process, Journal of Fluids Engineering ASME, 126, 210, 10.1115/1.1669032 Koefoed M.S, 2003. Modeling and Simulation of the VARTM Process for Wind Turbine Blades, Industrial Ph.D. Dissertation, Aalborg University. Kundan Kumar, 2013, Development of Vacuum Enhanced Resin Infusion Technology (VERITy) Process for Manufacturing of Primary Aircraft Structures, Journal of the Indian Institute of Science, 93 MIL-HDBK-17-5, “Composite Materials Handbook”. Ragondet A, 2005. Experimental Characterization of the Vacuum Infusion Process, PhD thesis, University of Nottingham. Ramesh Sundaram, KotreshM. Gaddikeri, Kundan Kumar Verma, Kailash Sing, Dinesh, B.L., & M. SubbaRao, “Tooling Concepts for Vacuum Enhanced Resin Infusion Technology (VERITy) Process”, INCCOM-5, November 2006. Tzetzis, 2008, Experimental and Finite Element Analysis on the Performance of Vacuum-assisted Resin Infused Single Scarf Repairs, Materials and Design, 29, 436, 10.1016/j.matdes.2007.01.002 Yosuke Nagao, Yutaka Iwahori, Yoshiyasu Hirano, Yuichro Aoki, 2005. “Low Cost Composite Wing Structure Manufacturing Technology Development Program in JAXA”, 16th international conference on composite materials SAMPE.