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Investigations into Load Spectra of UAVS Aircraft Cover

Investigations into Load Spectra of UAVS Aircraft

Open Access
|Aug 2014

References

  1. [1]. M. Rodzewicz, D. Glowacki Investigations into load spectrum and strength tests of an UAV structure, The READ 2012 Conference (Research and Education in Aircraft Design) – October 2012 Brno10.2478/v10164-012-0060-7
  2. [2]. M. Rodzewicz Determination and extrapolation of the glider load spectra. Volume 80 Issue 5 of Aircraft Engineering and Aerospace Technology, pp. 487 – 49610.1108/00022660810899856
  3. [3]. M. Rodzewicz Fatigue evaluation of high-loaded aeronautical composite structures. Aircraft Engineering and Aerospace Technology, Vol 81, No 5, pp 452 – 46010.1108/00022660910983743
  4. [4]. Rodzewicz M., Czerwiňski G., Kubica B. J.: Load spectrum – archiving, analysis and load sequences reproduction (in Polish), Proceedings of XIII Conf. Mechanics in Aviation, PTMTS ML-XIII 2008, vol. 1, pp.43 - 55
  5. [5]. Owczarek W., Rodzewicz M. Investigations into glider chassis load spectrum, Fatigue of Aircraft Structures Monographic Series, Issue 2009, pp 150 – 170.10.2478/v10164-010-0014-x
DOI: https://doi.org/10.2478/fas-2013-0004 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 40 - 52
Published on: Aug 21, 2014
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2014 Miroslaw Rodzewicz, Dominik Glowacki, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.