Crash concept for composite transport aircraft using mainly tensile and compressive absorption mechanisms

Author:

Schatrow PaulORCID,Waimer Matthias

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference48 articles.

1. Federal Aviation Administration: Special conditions: Boeing model B787-8 airplane; Crashworthiness. US Federal register vol. 72, No. 111, Docket No. NM368 Special Conditions No. 25-07-05-SC (2007)

2. Federal Aviation Administration: Special conditions: Airbus model A350-900 airplane; Crashworthiness. US Federal register vol. 79, No. 143, Docket No. FAA-2013-0892 Special Conditions No. 25-537-SC (2014)

3. Boitnott, R.L., Fasanella, E.L., Calton, L.E., Carden, H.D.: Impact response of composite fuselage frames. SAE Technical Paper 871009 (1987)

4. Boitnott, R.L., Fasanella, E.L.: Impact evaluation of composite floor sections. SAE Technical Paper 891018 (1989)

5. Waimer, M., Kohlgrüber, D., Keck, R., Voggenreiter, H.: Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup. CEAS Aeronaut. J. 4, 265–275 (2013)

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