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Influence of Honeycomb Core Stabilization on Composite Sandwich Structure Geometry Cover

Influence of Honeycomb Core Stabilization on Composite Sandwich Structure Geometry

Open Access
|Nov 2019

References

  1. [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.
  2. [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
  3. [3] Federal Aviation Administration, U.S. Department of Transportation, 1997, Handbook: Manufacturing Advanced Composite Components for Airframes.
  4. [4] Daniel G., 2014, Composite Materials: Design and Applications, Third Edition, CRC Press.
  5. [5] Baker, Alan A., 2004, Composite Materials for Aircraft Structures, AIAA.
  6. [6] Szymański, R., 2016, „Technologia Wykonania Noska Łopaty Wirnika Nośnego, Porównanie Trzech Technologii”, Prace Instytutu Lotnictwa, 244, pp. 155-166.10.5604/05096669.1222767
  7. [7] Kozaczuk, K., 2016, „Automated Fiber Placement Systems Overview”, Prace Instytutu Lotnictwa, 245, pp. 52-59.10.5604/05096669.1226355
  8. [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
Language: English
Page range: 1 - 13
Published on: Nov 8, 2019
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2019 Mateusz Michalski, Wojciech Krauze, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.