Workbench for the first stages of gas turbine engine compressors
<pre id="tw-target-text" class="tw-data-text tw-ta tw-text-small" dir="ltr"><span lang="en">The description of the structural features of the working shoulder blade with the inflow in the root portion and the results of the comparative numerical si...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aviation University
2002-04-01
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| Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
| Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/13605 |