Non-destructive evaluation of co-cured wing for SARAS

Srinivasa, V and Jangir, SC and Kumar, MR and Ramachandra, HV and Sudheendra, HN and Madhava, MR (2008) Non-destructive evaluation of co-cured wing for SARAS. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-024), 26-28 Jun 2008, Bangalore, India.

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Abstract

After considerable experience with the development of pre-preg based (mostly Fiberdux T300-914C) autoclave13; moulded carbon epoxy composite airworthy components for both Tejas (LCA) and SARAS programmes, the Advanced Composites Division (ACD) has now come out with an ingenious Vacuum Enhanced Resin Infusion Technology (VERITy) route for the development of Co-cured Carbon Wing for the SARAS aircraft using Carbon Fabric and Epoxy resin. Non-Destructive Evaluation (NDE) has played a crucial role in the formulation of the VERITy process. Also, NDE will be used in the qualification of the wing components and an approach has been evolved.

Item Type: Conference or Workshop Item (Paper)
Additional Information: Copyright for this article belongs to National Aerospace Laboratories
Uncontrolled Keywords: VERITy process;Non-destructive evaluation (NDE);SARAS wing
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 11 not found.
Date Deposited: 26 Feb 2009
Last Modified: 17 Jun 2010 08:50
URI: http://nal-ir.nal.res.in/id/eprint/4989

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