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The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure Cover

The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure

Open Access
|Jun 2016

References

  1. [1] Meteorologia dla pilotów–poradnik, Szefostwo Służby Meteorologicznej Sił Zbrojnych RP, Warszawa 2011.
  2. [2] G. Wypych, Handbook of Environmental Degradation of Materials, ChemTec Publishing, 2003, ISBN 1-895198-28-3
  3. [3] H. Gandy, „Adhesiveless Honeycomb Sandwich Structure With Carbon Graphite Prepreg For Primary Structural Application: A Comparative Study To The Use Of Adhesive Film” Thesis by H. Gandy, Wichita State University, 1999.
  4. [4] Choi H.S., Jang Y.H., Bondline strength evaluation of cocure/precured honeycomb sandwich structures under aircraft hygro and repair environments, Composites: Part A 41 (2010)10.1016/j.compositesa.2010.04.012
  5. [5] Ibarra-Castanedo C., Marcotte F., Genest M., Brault L., Farley V., Maldague X. P. V., Detection and characterization of water ingress in honeycomb structures by passive and active infrared thermography using a high resolution camera, 11th International Conference on Quantitative InfraRed Thermography 201210.1117/12.918567
  6. [6] Bartholomeusz R.A., Reduction of shear and flatwise tension strength in f-111 honeycomb panels exposed to moisture, DSTO-TR-1331, 1996
DOI: https://doi.org/10.1515/fas-2015-0004 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 24 - 27
Published on: Jun 30, 2016
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2016 Piotr Synaszko, Michał Sałaciński, Łukasz Kornas, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.