Thrust Performance and Heat Load Modelling of Pulse Detonation Engines
Pulse Detonation Engines (PDEs) are propulsion systems that use repeated detonations to generate thrust. Currently in early stages of development, PDEs have been theorised to have advantages over current deflagration based engines. Air-breathing PDEs could attain higher specific impulse values and o...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Institutionen för system- och rymdteknik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-82438 |