Glare Teardowns From the Megaliner Barrel (Mlb) Fatigue Test

Author:

Wanhill R. J. H.,Platenkamp D. J.,Hattenberg T.,Bosch A. F.,de Haan P. H.

Publisher

Springer Netherlands

Reference16 articles.

1. Wagner, M. (2001): Fatigue loads program for MegaLiner Barrel, Airbus Deutschland GmbH, Hamburg.

2. Platenkamp, D.J., Bosch, A.F., Wanhill, R.J.H., Hattenberg, T. (2005): MegaLiner Barrel teardown programme, Part I: NDI test results for the F4 window panel, NLR Contract Report NLR-CR-2005-665, National Aerospace Laboratory NLR, Amsterdam.

3. Wanhill, R.J.H., Hattenberg, T., Platenkamp, D.J., Bosch, A.F. (2006): MegaLiner Barrel teardown programme, Part II: fractographic examination and analysis of fatigue cracks for the F4 window panel, NLR Contract Report NLR-CR-2005-666, National Aerospace Laboratory NLR, Amsterdam.

4. Wanhill, R.J.H., Platenkamp, D.J., Hattenberg, T., Bosch, A.F. (2006): Teardown of a GLARE window area from the Airbus MegaLiner Barrel fatigue test article, NLR Technical Publication NLR-TP-2006-183, National Aerospace Laboratory NLR, Amsterdam.

5. Grooteman, F.P. (2005): Personal Communication, National Aerospace Laboratory NLR, Amsterdam.

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1. Experiment investigations of effect of laminate thickness on flexural properties of GLARE and GFRP laminates;Materials Research Express;2018-11-23

2. GLARE®: A Versatile Fibre Metal Laminate (FML) Concept;Aerospace Materials and Material Technologies;2016-11-12

3. Fatigue Requirements for Aircraft Structures;Aerospace Materials and Material Technologies;2016-11-08

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