An Analysis of Compressor Blade by Using a Digital Scanner
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001730" target="_blank" >RIV/00010669:_____/14:#0001730 - isvavai.cz</a>
Result on the web
<a href="http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" target="_blank" >http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
An Analysis of Compressor Blade by Using a Digital Scanner
Original language description
This paper describes dynamic analysis of the axial compressor first stage rotor blade of the jet engine Lyulka AL-7 without knowledge of the technical drawing. The work core point i.e. the non-contact blade measurement was performed by the use of an optical 3D scanner. The outcome of this work is in the comparison and evaluation of obtained results with previous analytical and numerical calculations of different authors and with their experimental measurements as well. The usefulness and accuracy of this method and procedure are evident.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
N - Vyzkumna aktivita podporovana z neverejnych zdroju
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
New Trends in Aviation Development 2014
ISBN
978-80-553-1650-5
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
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Publisher name
Faculty of Aeronautics, Technical University of Košice
Place of publication
Košice, Slovenská republika
Event location
Košice, Slovenská republika
Event date
Jan 1, 2014
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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