Integrity Evaluation of Feature Level Test Specimen of an Aircraft Primary Composite Structure

Author:

Venkatesh S.,Lakshminarayana S. C.,Varughese Byji

Publisher

Springer Singapore

Reference5 articles.

1. H.G.S.J. Thuis, C. Biemans, Design, fabrication and testing of a composite bracket for aerospace applications. Compos. Struct. 38(1–4), 91–98 (1997)

2. K.I. Tserpes, R. Ruzek, R. Mezihorak, G.N. Labeas, Sp.G. Pantelakis, The structural integrity of a novel composite adhesively bonded flap-track beam. Compos. Struct. 93, 2049–2059 (2011)

3. B. Ramanaiah, H.V. Ramachandra, S. Sanjeev Kumar, M.G. Kotresh, B. Varughese, R. Sundaram, Challenges in static testing of co-cured co-bonded composite aircraft structure, in National Conference on Scientific Achievements of SC & ST Scientists & Technologists, National Aerospace Laboratories, Bangalore-17, 14–16 Apr 2009

4. R.S. Lahey, M.P. Miller, M. Reymond, MSC/NASTRAN Version 70 Reference Manual (The MacNeal-Schwendler Corporation, 2003)

5. M.C.-Y. Niu, Airframe Stress Analysis & Sizing, 2nd edn. (Hong Kong Conmilit Press Ltd, Jan 1999)

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