Förbättrad förbränningsstabilitet i EBK för turbofläktmotor RM12 genom förändrad motorreglering : Improved afterburner combustion stability for turbofan engine RM12 by modified engine control
The engine of JAS 39 Gripen, RM12, has recently been equipped with a new flameholder and a new engine inlet. This change has caused an increased noise level from the engine when the afterburner is in use. The noise level reaches its peak when the afterburner is partially used. The problem is thought...
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| Format: | Others |
| Language: | Swedish |
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Linköpings universitet, Institutionen för systemteknik
2005
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-282 |