New model of work of the gas-turbine engine
<p><em> Problem questions of the gas-turbine engines exploitation are analysed. It is shown, that the gas-mechanics regulation of aerodynamic profile attack corner theorem allowed to design the regulation of the axial compressor system. This system is ability to provide reliable function...
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| Format: | Article |
| Language: | English |
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National Aviation University
2004-04-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/1078 |
| Summary: | <p><em> Problem questions of the gas-turbine engines exploitation are analysed. It is shown, that the gas-mechanics regulation of aerodynamic profile attack corner theorem allowed to design the regulation of the axial compressor system. This system is ability to provide reliable functioning of the gas-turbine engine at any service conditions.</em></p> |
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| ISSN: | 1813-1166 2306-1472 |