PIK-20D Glider Fatigue Review
Abstract
A fatigue inspection program has been established for the PIK-20D glider. This paper explains the reasoning for the inspection interval and the inspection objects. As a basis for this the stress calculations, fatigue and material tests and drawings of PIK-20D were reviewed. A noticeable effort was made to collect all relevant material data derived in the 1970s. The fatigue calculations performed were reviewed and the results were transformed to be consistent with the Kossira-Reinke spectrum, which has become a standard in Europe. The effect of aerobatic flight on fatigue was investigated. The review covers the entire glider with emphasis on the wing composite spar and web and the primary metal brackets. The review shows a long fatigue life and that there are no known fatigue problems on PIK-20D.
Downloads
Published
Issue
Section
License
CLEARANCE AND LICENSE TO PUBLISH:
This paper is UNCLASSIFIED (for public reasons) and has been cleared by the appropriate agencies, company and government. This paper represents original work by the author(s). No portion of the material is covered by a prior copyright; or for any portion copyrighted, the author has obtained permission for its use.
I hereby license OSTIV to publish this paper and to use it for all of OSTIV's current and future publications uses.