A Test Concept For Future Aircraft Fuselage Panels

Author:

Best R.,Fleischer Th.,Götze M.,Sachse M.,Semsch M.

Publisher

Springer Netherlands

Reference4 articles.

1. B. Borgonje, M. Escobedo Medina (2007) in: Lessons learnt from the Full-Scale Fatigue Test ‘Megaliner Barrel’ — F&DT Analysis of the Glare Structure, Proceedings of the 24th ICAF Symposium, vol. I, p. 400, L. Lazzeri and A. Salvetti (Ed.), Publ. Pacini, Naples

2. L. le Tellier, F. Repiton (2007) in: Full-scale testing and analysis of Falcon 7X curved fuselage panels with Butt-joints, Proceedings of the 24th ICAF Symposium, vol. I, p. 340, L. Lazzeri and A. Salvetti (Ed.), Publ. Pacini, Naples

3. D. R. Ambur, J. A. Cerrof, J. Dickson (1995) in: D-Box Fixture for Testing Stiffened Panels in Compression and Pressure, AIAA Journal of Aircraft, vol. 32–6, p. 1382

4. R. W. A. Vercammen, H. H. Ottens (1998) in: Full-scale fuselage panel tests, Proceedings of the 21st ICAS Congress, TP 98148

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