Literature
169
[Dav08]
Davies, G. A. O.; Ankersen, J.: „Virtual testing of realistic aerospace
composite structures“, in: Journal of Materials Science, 2008, 43; S.
6586–6592.
[Dem01]
Demelio, G.; Genovese, K.; Pappalettere, C.: „An experimental investigation of static and fatigue behaviour of sandwich composite panels
joined by fasteners“, in: Composites Part B: Engineering, 2001, 32; S.
299–308.
[DIN291]
Deutsches Institut für Normung: „DIN 53291 Testing of sandwiches;
Compression test perpendicular to the faces“. Beuth Verlag, Berlin,
1982.
[DIN292]
Deutsches Institut für Normung: „DIN 53292 Testing of sandwiches;
Tensile test perpendicular to the faces“. Beuth Verlag, Berlin, 1982.
[DIN294]
Deutsches Institut für Normung: „DIN 53294 Testing of sandwiches;
Shear test“. Beuth Verlag, Berlin, 1982.
[DuP03]
DuPont: „Nomex - technical data sheet“. E.I. du Pont de Nemours and
Company, 2003.
[EAS17]
EASA: „CS 25 - Certification Specifications and Acceptable Means of
Compliance for Large Aeroplanes - Amendment 20“. Amendment 20,
2017.
[ESA11]
ESA: „Space engineering Insert Design Handbook“, 2011.
[EUR10]
EURO-COMPOSITES: „Mechanical PropertiesECA Honeycomb (metrical,
test specimen thickness 12.7 mm)“, 2010.
[Fel09]
Feldhusen, J.; Warkotsch, C.; Kempf, A.: „Development of a Mechanical
Technology for Joining Sandwich Elements“, in: Journal of Sandwich
Structures & Materials, 2009, 11; S. 471–486.
[Fis09]
Fischer, S.; Drechsler, K.; Kilchert, S.; Johnson, A.: „Mechanical tests for
foldcore base material properties“, in: Composites Part A: Applied Science and Manufacturing, 2009, 40; S. 1941–1952.
[Fis16]
Fischer, C.; Hähnel, F.; Hauffe, A.; Wolf, K.: „Influence of Imperfections
on the Structural Behaviour of Honeycomb Cores“, in: 17th European
Conference on Composite Materials, 2016, 26 - 30 June - Munich, Germany.