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In-Service Flaw Detection and Quantification in the Composite Structures of Aircraft Cover

In-Service Flaw Detection and Quantification in the Composite Structures of Aircraft

Open Access
|Sep 2010

References

  1. FAA. (2000, January). Probabilistic Design of Damage Tolerant Composite Aircraft Structures. Office of Aviation Research Washington. (DOT/FAA/AR-01/55)
  2. Dragan, K., & Klimaszewski, S. (2006) In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin. In: Proceedings of the 9th European Conference on Non Destructive Testing, 25-29 September 2006, Berlin.
  3. Dragan, K., & Klimaszewski, S. (2008). Holistic Approach for Structural Integrity Evaluation of Composite Main Rotor Blades. In: Proceedings of the 17th World Conference on Non Destructive Testing, 26-31 August 2008, Shanghai.
  4. Synaszko, P., Dragan, K., & Salacinski, M. (2008). Badania nieniszczące kompozytowych struktur szybowca PW-5. In: Proceedings of the 37th National Conference on Non-Destructive Testing, 21-23 October 2008, Sobieszewo.
  5. Roach, D. (2007, January). Smart Aircraft Structures: a Future Necessity. High Performance Composites, 15(1), 28-30.
DOI: https://doi.org/10.2478/v10164-010-0003-0 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 37 - 41
Published on: Sep 23, 2010
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2010 Krzysztof Dragan, Piotr Synaszko, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2009 (2009): Issue 1 (July 2009)