OPTIMIZATION OF NOZZLE SETTINGS FOR A FIGHTER AIRCRAFT
Most fighters use the convergent-divergent nozzle configuration to accelerate into the supersonic realm. This nozzle configuration greatly increases the thrust potential of the aircraft compared to the simpler convergent nozzle. The nozzle design is not only crucial for thrust, but also for the drag...
| Main Authors: | , |
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| Format: | Others |
| Language: | English |
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Mälardalens högskola, Industriell ekonomi och organisation
2019
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| Subjects: | |
| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-45487 |