Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation
In the paper short information about advantages of introduction of detonation combustion to propulsion systems is briefly discussed and then research conducted at the Łukasiewicz-Institute of Aviation on development of the rotating detonation engines (RDE) is presented. Special attention is focused...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
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Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines
2022-01-01
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| Series: | Combustion Engines |
| Subjects: | |
| Online Access: | http://www.combustion-engines.eu/Applications-of-the-continuously-rotating-detonation-to-combustion-engines-at-the,145409,0,2.html |
| _version_ | 1797964749094256640 |
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| author | Michał Cezary Kawalec Witold Perkowski Borys Łukasik Adam Bilar Piotr Wolański |
| author_facet | Michał Cezary Kawalec Witold Perkowski Borys Łukasik Adam Bilar Piotr Wolański |
| author_sort | Michał Cezary Kawalec |
| collection | DOAJ |
| description | In the paper short information about advantages of introduction of detonation combustion to propulsion systems is briefly discussed and then research conducted at the Łukasiewicz-Institute of Aviation on development of the rotating detonation engines (RDE) is presented. Special attention is focused on continuously rotating detonation (CRD), since it offers significant advantages over pulsed detonation (PD). Basic aspects of initiation and stability of the CRD are discussed. Examples of applications of the CRD to gas turbine and rocket engines are presented and a combine cycle engine utilizing CRD are also evaluated. The world's first rocket flight powered by liquid propellant detonation engine is also described. |
| first_indexed | 2024-04-11T01:49:52Z |
| format | Article |
| id | doaj.art-6a8149d40ce0448eb4488b7811a80d65 |
| institution | Directory Open Access Journal |
| issn | 2300-9896 2658-1442 |
| language | English |
| last_indexed | 2024-04-11T01:49:52Z |
| publishDate | 2022-01-01 |
| publisher | Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines |
| record_format | Article |
| series | Combustion Engines |
| spelling | doaj.art-6a8149d40ce0448eb4488b7811a80d652023-01-03T06:56:34ZengPolskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion EnginesCombustion Engines2300-98962658-14422022-01-011914515710.19206/CE-145409145409Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of AviationMichał Cezary Kawalec0https://orcid.org/0000-0003-3147-3516Witold Perkowski1https://orcid.org/0000-0002-7580-5319Borys Łukasik2https://orcid.org/0000-0003-4512-2880Adam Bilar3https://orcid.org/0000-0001-9479-5075Piotr Wolański4https://orcid.org/0000-0003-3963-7722Aircraft Propulsion Systems Department Unmanned Technology Centre, Lukasiewicz Research Center- Institute of Aviation, PolandAircraft Propulsion Systems Department Unmanned Technology Centre, Lukasiewicz Research Center- Institute of Aviation, PolandAircraft Propulsion Systems Department Unmanned Technology Centre, Lukasiewicz Research Center- Institute of Aviation, PolandAircraft Propulsion Systems Department Unmanned Technology Centre, Lukasiewicz Research Center- Institute of Aviation, PolandAircraft Propulsion Systems Department Unmanned Technology Centre, Lukasiewicz Research Center- Institute of Aviation, PolandIn the paper short information about advantages of introduction of detonation combustion to propulsion systems is briefly discussed and then research conducted at the Łukasiewicz-Institute of Aviation on development of the rotating detonation engines (RDE) is presented. Special attention is focused on continuously rotating detonation (CRD), since it offers significant advantages over pulsed detonation (PD). Basic aspects of initiation and stability of the CRD are discussed. Examples of applications of the CRD to gas turbine and rocket engines are presented and a combine cycle engine utilizing CRD are also evaluated. The world's first rocket flight powered by liquid propellant detonation engine is also described.http://www.combustion-engines.eu/Applications-of-the-continuously-rotating-detonation-to-combustion-engines-at-the,145409,0,2.htmldetonationrdedetonation enginesexperimental rocket |
| spellingShingle | Michał Cezary Kawalec Witold Perkowski Borys Łukasik Adam Bilar Piotr Wolański Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation Combustion Engines detonation rde detonation engines experimental rocket |
| title | Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation |
| title_full | Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation |
| title_fullStr | Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation |
| title_full_unstemmed | Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation |
| title_short | Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz - Institute of Aviation |
| title_sort | applications of the continuously rotating detonation to combustion engines at the lukasiewicz institute of aviation |
| topic | detonation rde detonation engines experimental rocket |
| url | http://www.combustion-engines.eu/Applications-of-the-continuously-rotating-detonation-to-combustion-engines-at-the,145409,0,2.html |
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