Peculiarity of simulation of transitional processes on turbo fan engine with mixed flows
<span lang="EN-US">Considered is a particular simulation of transitional process on turbo fan engine with mixed flows. The given models allow to define engine compressor working lines for uprated checking fitness according to parameter readings of airborne registration systems</sp...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aviation University
2000-09-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/9696 |
| Summary: | <span lang="EN-US">Considered is a particular simulation of transitional process on turbo fan engine with mixed flows. The given models allow to define engine compressor working lines for uprated checking fitness according to parameter readings of airborne registration systems</span> |
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| ISSN: | 1813-1166 2306-1472 |