192
Appendix B – Structural element level
Appendix B – Structural element level
B1 Sandwich bending test details
Notation
t [mm]
b [mm] l [mm]
Failure
B19-L101_01
19.5
50.1
250
Compressive face sheet rupture
B19-L101_02
19.5
50.1
250
Compressive face sheet rupture
B19-L101_03
19.4
50.1
250
Local core indentation
B19-W101_01
19.5
50.1
250
Local core indentation
B19-W101_02
19.4
50.1
250
Local core indentation
B19-W101_03
19.4
50.1
250
Local core indentation
B26-L101_01
26.3
49.2
250
Local core indentation
B26-L101_02
26.3
49.2
250
Local core indentation
B26-W101_01
26.3
49.2
250
Local core indentation
B26-W101_02
26.3
49.2
250
Local core indentation
B19-L003_01
19.3
50.2
250
Local core indentation
B19-L003_02
19.2
50.1
250
Local core indentation
B19-L003_03
19.2
50.2
250
Local core indentation
B19-W003_01
19.2
50.1
250
Core shear
B19-W003_02
19.3
50.1
250
Core shear
B19-W003_03
19.3
50.1
250
Core shear
© Springer-Verlag GmbH Germany, part of Springer Nature 2020
R. Seemann, A Virtual Testing Approach for Honeycomb Sandwich Panel
Joints in Aircraft Interior, Produktentwicklung und Konstruktionstechnik 16,
https://doi.org/10.1007/978-3-662-60276-8