Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup

Author:

Waimer M.,Kohlgrüber D.,Keck R.,Voggenreiter H.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference19 articles.

1. Federal Aviation Administration: Special conditions—Boeing model 787-8 airplane—crashworthiness, US federal register, 72(111), (2007) Docket No. NM368 special conditions No. 25-07-05-SC

2. Le Page, F., Carciente, R.: A320 fuselage section vertical drop test—part 2: test results, CEAT test report N° S95 5776/2, European project ‘Crashworthiness for Commercial Aircraft’ (1995)

3. Kumakura, I., Sashikuma, H., et al.: Summary of vertical drop tests of YS-11 transport fuselage sections, SAE technical paper 2003-01-3027 (2003)

4. Abramowitz, A., Smith, T.G., Vu, T.: Vertical drop test of a narrow-body transport fuselage section with a conformable auxiliary fuel tank onboard, DOT/FAA/AR-00/56 (2000)

5. Abramowitz, A., Smith, T.G., Vu, T., Zvanya J.R.: Vertical drop test of a narrow-body transport fuselage section with overhead stowage bins, DOT/FAA/AR-01/100 (2002)

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