Proceedings Vol. 9 (2003)
ENGINEERING MECHANICS 2003
May 11 – 15, 2003, Svratka, Czech Republic
Copyright © 2003 Institute of Theoretical and Applied Mechanics, Academy of Sciences of the Czech Republic, v.v.i., Prague
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 68 - +7p., full text
The crack growth prediction techniques in the critical area of the small transport aircraft undercarriage bracket has been describe in this paper. Stress-state was determined by FEM numerical simulation. The PREDIKCE code was used for crack growth curve determination. This code was developed in the Aeronautical Research and Test Institute (VZLU). The crack initial size was determined based on experimental data and computation.
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