The shape and dimensions of flame stabilizers of a direct-flow type combustion chamber influence on the hydraulic characteristics
Direct-flow combustion chambers are afterburner combustion chambers, which are used to short-term increase the thrust of a gas turbine engine for takeoff, maneuvering and overcoming the sound barrier by an aircraft and its flight at supersonic speed. Also, direct-flow combustion chambers are used as...
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| Format: | Article |
| Language: | English |
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National Aerospace University «Kharkiv Aviation Institute»
2022-08-01
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| Series: | Авіаційно-космічна техніка та технологія |
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| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1762 |