ERROR ANALYSIS OF THERMOCOUPLE DYNAMIC PERFORMANCES EXPERIMENTAL DETERMINING IN ENGINE CONDITIONS USING STEP RESPONCE
The turbine inlet temperature is one of the major thermodynamic parameters that determine specific thrust and specific fuel consumption of the turbine engine. The gas temperature also influences the temperature of the engine parts, hence thermal stresses and the ability of materials to support stati...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aerospace University «Kharkiv Aviation Institute»
2020-08-01
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| Series: | Авіаційно-космічна техніка та технологія |
| Subjects: | |
| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1213 |