INVESTIGATION OF COOLING PERFORMANCES AT THE GAS TURBINE BLADE CHANNEL
The cooling of the turbine blades in different parts of the turbine is carried out using different cooling techniques. Approximately 20% of the air produced in compressors is used in cooling systems. The air is sent into the wing through the internal channels. It travels through the outer profile of...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Hezarfen Aeronautics and Space Technologies Institue
2014-07-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/74/69 |