The Cracks Propagation Calculations in the PZL-130 Orlik Structure
By: Marcin Kurdelski and Łukasz Obrycki
Open Access
|Dec 2010Abstract
The article presents the results of research carried out under a research project on the evaluation of fatigue life. The subject of the analysis was the critical elements of the PZL-130 Orlik. The numerical crack growth analyses were performed using the NASGRO equation. The Orlik aircraft are mainly used for the basic pilot training in the Polish Air Force. Each airplane is equipped with a digital flight data recorder. The record of more than 36000 flight hours is the basis for numerical analysis of fatigue life.
DOI: https://doi.org/10.2478/v10164-010-0026-6 | Journal eISSN: 2300-7591
Language: English
Page range: 59 - 68
Published on: Dec 20, 2010
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
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© 2010 Marcin Kurdelski, Łukasz Obrycki, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.