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Airworthiness Tests of the UAV Structure − Fatigue Issues Cover

Airworthiness Tests of the UAV Structure − Fatigue Issues

Fatigue of Aircraft Structures
Volume 2012 (2012): Issue 4 (December 2012)
By: Mirosław Rodzewicz  
Open Access
|Apr 2013

References

  1. [1] Rodzewicz, M. Determination and extrapolation of the glider load spectra. AircraftEngineering and Aerospace Technology, Vol. 80(5), pp. 487-496.10.1108/00022660810899856
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  2. [2] Rodzewicz, M. Fatigue evaluation of high-loaded aeronautical composite structures. AircraftEngineering and Aerospace Technology, Vol. 81(5), pp. 452-460.10.1108/00022660910983743
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  3. [3] Rodzewicz M., Czerwiński 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.
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  4. [3] Owczarek W., Rodzewicz M. (2009). Investigations into glider chassis load spectrum, Fatigue of Aircraft Structures Monographic Series, Issue 2009, pp. 150-170.
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DOI: https://doi.org/10.2478/v10164-012-0060-7 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 82 - 93
Published on: Apr 30, 2013
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
UAV loads,
load spectrum,
manual control,
autopilot
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2013 Mirosław Rodzewicz, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

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