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 (supervisor 1)
W.P.J. Visser (supervisor 1)
P.C. Roling (supervisor 1)
E.R. Rademaker (supervisor 1)
Faculty
Aerospace Engineering
Copyright: © 2018 Michelle Jagtenberg
Heat transfer Gas turbine Lifing analysis
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Published Date

19-02-2018

Language

English

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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.