Profitability of the gas-turbine engine with two-row blade wreaths in the axial compressor
<p><em> The way of the solution of increasing effectivity gas turbine engine problem is considered. Results of researches of the axial compressor stage with constant circulation are submitted. Recommendations for profiling two-row blade rings are developed on the basis of use of eject...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aviation University
2005-04-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/1244 |