172
Literature
[Joh01]
Johnson, A. F.: „Modelling fabric reinforced composites under impact
loads“, in: Composites Part A: Applied Science and Manufacturing,
2001, 32; S. 1197–1206.
[Joh15]
Johnson, A. F.; Thomson, R. S.; David, M.; Joosten, M. W.: „Design and
testing of crashworthy aerospace composite components“, in: Polymer
Composites in the Aerospace Industry, 2015; S. 261–293.
[Kar13]
Karakoç, A.; Santaoja, K.; Freund, J.: „Simulation experiments on the effective in-plane compliance of the honeycomb materials“, in: Composite Structures, 2013, 96; S. 312–320.
[Kil13]
Kilchert, S.: „Nonlinear finite element modelling of degradation and failure in folded core composite sandwich structures“. Dissertation, DLR,
Bibliotheks- und Informationswesen, Köln, 2013.
[Kim08]
Kim, B. J.; Lee, D. G.: „Characteristics of joining inserts for composite
sandwich panels“, in: Composite Structures, 2008, 86; S. 55–60.
[Kim97]
Kim, D.S. and Lee, J.R.: „Compressive Mechanical Properties of the
Nomex/Thermoset Honeycomb Cores“, in: Polymers for Advanced
Technologies, 1997, 8; S. 1–7.
[Kr16]
Krause, D.; Seemann, R.; Oltmann, J.; Rasmussen, O.: „Produktvalidierung von Leichtbaustrukturen für die Flugzeugkabine“, in: 65. Deutscher
Luft- und Raumfahrtkongress, 2016, Braunschweig.
[Lam17]
Laminated Plastics: „Technical Data Sheet - Linen Phenolic -
http://www.laminatedplastics.com/“. http://www.laminatedplastics.com/, Billerica, MA, 2017.
[Lim11]
Lim, J. W.; Lee, D. G.: „Development of the hybrid insert for composite
sandwich satellite structures“, in: Composites Part A: Applied Science
and Manufacturing, 2011, 42; S. 1040–1048.
[Liu03]
Liu, G. R.; Quek, S. S.: „The finite element method - A practical course“.
Butterworth-Heinemann, Oxford, Boston, 2003.
[Liu15]
Liu, L.; Wang, H.; Guan, Z.: „Experimental and numerical study on the
mechanical response of Nomex honeycomb core under transverse loading“, in: Composite Structures, 2015, 121; S. 304–314.
[Liu15]
Liu, L.; Meng, P.; Wang, H.; Guan, Z.: „The flatwise compressive properties of Nomex honeycomb core with debonding imperfections in the
Literature
[Joh01]
Johnson, A. F.: „Modelling fabric reinforced composites under impact
loads“, in: Composites Part A: Applied Science and Manufacturing,
2001, 32; S. 1197–1206.
[Joh15]
Johnson, A. F.; Thomson, R. S.; David, M.; Joosten, M. W.: „Design and
testing of crashworthy aerospace composite components“, in: Polymer
Composites in the Aerospace Industry, 2015; S. 261–293.
[Kar13]
Karakoç, A.; Santaoja, K.; Freund, J.: „Simulation experiments on the effective in-plane compliance of the honeycomb materials“, in: Composite Structures, 2013, 96; S. 312–320.
[Kil13]
Kilchert, S.: „Nonlinear finite element modelling of degradation and failure in folded core composite sandwich structures“. Dissertation, DLR,
Bibliotheks- und Informationswesen, Köln, 2013.
[Kim08]
Kim, B. J.; Lee, D. G.: „Characteristics of joining inserts for composite
sandwich panels“, in: Composite Structures, 2008, 86; S. 55–60.
[Kim97]
Kim, D.S. and Lee, J.R.: „Compressive Mechanical Properties of the
Nomex/Thermoset Honeycomb Cores“, in: Polymers for Advanced
Technologies, 1997, 8; S. 1–7.
[Kr16]
Krause, D.; Seemann, R.; Oltmann, J.; Rasmussen, O.: „Produktvalidierung von Leichtbaustrukturen für die Flugzeugkabine“, in: 65. Deutscher
Luft- und Raumfahrtkongress, 2016, Braunschweig.
[Lam17]
Laminated Plastics: „Technical Data Sheet - Linen Phenolic -
http://www.laminatedplastics.com/“. http://www.laminatedplastics.com/, Billerica, MA, 2017.
[Lim11]
Lim, J. W.; Lee, D. G.: „Development of the hybrid insert for composite
sandwich satellite structures“, in: Composites Part A: Applied Science
and Manufacturing, 2011, 42; S. 1040–1048.
[Liu03]
Liu, G. R.; Quek, S. S.: „The finite element method - A practical course“.
Butterworth-Heinemann, Oxford, Boston, 2003.
[Liu15]
Liu, L.; Wang, H.; Guan, Z.: „Experimental and numerical study on the
mechanical response of Nomex honeycomb core under transverse loading“, in: Composite Structures, 2015, 121; S. 304–314.
[Liu15]
Liu, L.; Meng, P.; Wang, H.; Guan, Z.: „The flatwise compressive properties of Nomex honeycomb core with debonding imperfections in the