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...
Main Author: | |
---|---|
Format: | Article |
Language: | English |
Published: |
National Aviation University
2004-04-01
|
Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/1078 |