176
Literature
[See17]
Seemann, R.; Krause, D.: „Numerical modelling of Nomex honeycomb
sandwich cores at meso-scale level“, in: Composite Structures, 2017,
159; S. 702–718.
[See18]
Seemann, R.; Krause, D.: „Numerical modelling of partially potted inserts in honeycomb sandwich panels under pull-out loading“, in: Composite Structures, 2018, 203; S. 101–109.
[Sei06]
Seibert, H. F.: „Applications for PMI foams in aerospace sandwich structures“, in: Reinforced Plastics, 2006, 50; S. 44–48.
[Shu96]
Shur-Lok Corporation: „Design Manual Fasteners for Sandwich Structure“, Irvine, CA, 1996.
[Sil05]
da Silva, Lucas F. M.; Adams, R. D.: „Measurement of the mechanical
properties of structural adhesives in tension and shear over a wide
range of temperatures“, in: Journal of Adhesion Science and Technology, 2005, 19; S. 109–141.
[Sli17]
Slimane, S.; Kebdani, S.; Boudjemai, A.; Slimane, A.: „Effect of position
of tension-loaded inserts on honeycomb panels used for space applications“, in: International Journal on Interactive Design and Manufacturing (IJIDeM), 2017, 16; S. 131.
[Smi12]
Smith, B.; Banerjee, B.: „Reliability of inserts in sandwich composite
panels“, in: Composite Structures, 2012, 94; S. 820–829.
[Son08]
Song, K.-I.; Choi, J.-Y. et al.: „An experimental study of the insert joint
strength of composite sandwich structures“, in: Composite Structures,
2008, 86; S. 107–113.
[Sta06]
Staal, R. A.: „Failure of sandwich honeycomb panels in bending“. PhD
Thesis. The University of Auckland, Auckland, 2006.
[Ste16]
Steenackers, G.; Peeters, J.; Ribbens, B.; Vuye, C.: „Development of an
Equivalent Composite Honeycomb Model - A Finite Element Study“. A
Finite Element Study, in: Applied Composite Materials, 2016, 23; S.
1177–1194.
[Tar04]
Tarantola, A.: „Inverse problem theory and methods for model parameter estimation“. Books24x7.com, Norwood Mass., 2004.
[Tay10]
Taylor, J. G.: „Composites“, in: Phenolic resins. A century of progress.
Springer, Heidelberg [Germany], London, New York, 2010; S. 263–306.
Literature
[See17]
Seemann, R.; Krause, D.: „Numerical modelling of Nomex honeycomb
sandwich cores at meso-scale level“, in: Composite Structures, 2017,
159; S. 702–718.
[See18]
Seemann, R.; Krause, D.: „Numerical modelling of partially potted inserts in honeycomb sandwich panels under pull-out loading“, in: Composite Structures, 2018, 203; S. 101–109.
[Sei06]
Seibert, H. F.: „Applications for PMI foams in aerospace sandwich structures“, in: Reinforced Plastics, 2006, 50; S. 44–48.
[Shu96]
Shur-Lok Corporation: „Design Manual Fasteners for Sandwich Structure“, Irvine, CA, 1996.
[Sil05]
da Silva, Lucas F. M.; Adams, R. D.: „Measurement of the mechanical
properties of structural adhesives in tension and shear over a wide
range of temperatures“, in: Journal of Adhesion Science and Technology, 2005, 19; S. 109–141.
[Sli17]
Slimane, S.; Kebdani, S.; Boudjemai, A.; Slimane, A.: „Effect of position
of tension-loaded inserts on honeycomb panels used for space applications“, in: International Journal on Interactive Design and Manufacturing (IJIDeM), 2017, 16; S. 131.
[Smi12]
Smith, B.; Banerjee, B.: „Reliability of inserts in sandwich composite
panels“, in: Composite Structures, 2012, 94; S. 820–829.
[Son08]
Song, K.-I.; Choi, J.-Y. et al.: „An experimental study of the insert joint
strength of composite sandwich structures“, in: Composite Structures,
2008, 86; S. 107–113.
[Sta06]
Staal, R. A.: „Failure of sandwich honeycomb panels in bending“. PhD
Thesis. The University of Auckland, Auckland, 2006.
[Ste16]
Steenackers, G.; Peeters, J.; Ribbens, B.; Vuye, C.: „Development of an
Equivalent Composite Honeycomb Model - A Finite Element Study“. A
Finite Element Study, in: Applied Composite Materials, 2016, 23; S.
1177–1194.
[Tar04]
Tarantola, A.: „Inverse problem theory and methods for model parameter estimation“. Books24x7.com, Norwood Mass., 2004.
[Tay10]
Taylor, J. G.: „Composites“, in: Phenolic resins. A century of progress.
Springer, Heidelberg [Germany], London, New York, 2010; S. 263–306.