Stress Analysis of the PZL M28’s Airframe Subjected to Repairs During Fatigue Tests
Brzęczek Józef, Gruszecki Henryk, Pieróg Leszek and 2 more
Fatigue of Aircraft Structures · 2014
doi:10.1515/fas-2014-0011 (opens in a new tab)
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Abstract
The PZL M28’s service life is determined based on the fatigue tests of the wing and wing loads-carry-through structure. During the fatigue test, the first occurrence of significance was the appearance of a in the area of the wing where loads are applied from the strut. It was demonstrated during further activities that repairs of the wing and other basic assemblies enabled, when performed at an appropriate time, the airplane’s service life to be significantly increase.
Abstract licence: CC BY
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