System development to determine blade tip running clearances in a jet engine high pressure compressor

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Volume Title

School of Engineering | Master's thesis
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Authors

Date

2012

Department

Sovelletun mekaniikan laitos

Major/Subject

Lentotekniikka

Mcode

Kul-34

Degree programme

Language

en

Pages

xiii + 93 s. + liitt.

Series

Description

Supervisor

Saarela, Olli

Thesis advisor

Knappett, Daniel

Keywords

tip clearance, suihkumoottori, high pressure compressor, kärkivälys, jet engine, optinen mittausmenetelmä, gas turbine

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Citation

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https://urn.fi/URN:NBN:fi:aalto-2020122858910

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[dipl] Insinööritieteiden korkeakoulu / ENG