Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine

Master thesis (2018)

Authors

M.H. Jagtenberg Aerospace Engineering

Contributors

Piero Colonna (mentor)
W.P.J. Visser (mentor)
P.C. Roling (mentor)
E.R. Rademaker (mentor)
Faculty
Aerospace Engineering, Aerospace Engineering
Copyright: © 2018 Michelle Jagtenberg
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Published Date

19-02-2018

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Abstract

In the near future the Royal Netherlands Air Force will replace their fleet of F-16’s with the F-35. In the past the NLR has aided the Air Force with life cycle and deterioration analysis work on the F100-PW-220 engine, which powers the F-16. Understanding the physical system of the engine allows for on-condition maintenance. The same is preferred for the F135-PW-100 engine powering the F-35. Therefore, a preliminary lifing analysis tool has been developed for the F135-PW-100 engine rotor blades, based on open source literature.