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Influence of Honeycomb Core Stabilization on Composite Sandwich Structure Geometry


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[1] Herrmann A.S., Zahlen P.C., Zuardy I., 2005, Sandwich Structures Technology in Commercial Aviation. In: Thomsen O., Bozhevolnaya E., Lyckegaard A. (eds) Sandwich Structures 7: Advancing with Sandwich Structures and Materials. Springer, Dordrecht. Search in Google Scholar

[2] Dirk H.-J.A. Lukaszewicz, Carwyn Ward, Kevin D. Potter, The engineering aspects of automated prepreg layup: History, present and future, Composites Part B: Engineering, 43(3), pp. 997-1009.10.1016/j.compositesb.2011.12.003 Search in Google Scholar

[3] Federal Aviation Administration, U.S. Department of Transportation, 1997, Handbook: Manufacturing Advanced Composite Components for Airframes. Search in Google Scholar

[4] Daniel G., 2014, Composite Materials: Design and Applications, Third Edition, CRC Press. Search in Google Scholar

[5] Baker, Alan A., 2004, Composite Materials for Aircraft Structures, AIAA. Search in Google Scholar

[6] Szymański, R., 2016, „Technologia Wykonania Noska Łopaty Wirnika Nośnego, Porównanie Trzech Technologii”, Prace Instytutu Lotnictwa, 244, pp. 155-166.10.5604/05096669.1222767 Search in Google Scholar

[7] Kozaczuk, K., 2016, „Automated Fiber Placement Systems Overview”, Prace Instytutu Lotnictwa, 245, pp. 52-59.10.5604/05096669.1226355 Search in Google Scholar

[8] Krauze, W., 2016, „Modern Process of Composite Structures Manufacturing Based on CAD Definition of the Composite”, Prace Instytutu Lotnictwa, 245, pp. 70-78.10.5604/05096669.1226426 Search in Google Scholar

eISSN:
2545-2835
Language:
English
Publication timeframe:
4 times per year
Journal Subjects:
Engineering, Introductions and Overviews, other, Geosciences, Materials Sciences, Physics