Мақаланы E-mail арқылы жіберу On the mechanism of aeroacoustic initiation of pulsed quasi-detonation combustion in an air-breathing ejector pulsejet
- Авторлар: Migalin K.V.1, Sidenko K.A.2
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Мекемелер:
- LLC Scientific-Production Company “Rotor”
- Togliatti State University
- Шығарылым: Том 15, № 3 (2022)
- Беттер: 88-99
- Бөлім: Articles
- URL: https://ogarev-online.ru/2305-9117/article/view/286661
- DOI: https://doi.org/10.30826/CE22150309
- EDN: https://elibrary.ru/KIEWCR
- ID: 286661
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
The present paper discusses the design of a pulse-jet engine in which a new mechanism of deflagration-to-detonation transition and establishment of a mode close to the detonation combustion or quasi-detonation mode is realized. It is found that the possibility of such a transition is provided by a special design of the gas duct which has a double bend leading to the formation of a specific vortex structure of the internal flow allowing the acoustic tuning of the gas duct to reach such combustion modes.
Авторлар туралы
Konstantin Migalin
LLC Scientific-Production Company “Rotor”
Хат алмасуға жауапты Автор.
Email: MigalinK7@gmail.com
Candidate of Science in technology, director
Ресей, TogliattiKirill Sidenko
Togliatti State University
Email: mail.ru63@mail.ru
student
Ресей, TogliattiӘдебиет тізімі
- Frolov, S. M., ed. 2006. Impul’snye detonatsionnye dvigateli [Pulse detonation engines]. Мoscow: TORUS PRESS. 592 p.
- Frolov, S. M., V. S. Aksenov, V. S. Ivanov, I. O. Shamshin, and S.A. Nabatnikov. 2019. Broskovye ispytaniya bespilot- nogo letatel’nogo apparata s pryamotochnym vozdushno- reaktivnym impul’sno-detonatsionnym dvigatelem [Catapult launching tests of an unmanned aerial vehicle with a ramjet pulsed-detonation engine]. Goren. Vzryv (Mosk.) — Combustion and Explosion 12(1):63–72.
- Migalin, K. V., K. A. Sidenko, and K. K. Migalin. 2020. Ezektornye pul’siruyushchie vozdushno-reaktivnye dvigateli [Ejector pulsed air jet engines]. Togliatti: Spectrum Publishing House. 444 p.
- Migalin, K. V., and K.A. Sidenko. 2021. O razrabotke vozdushno-reaktivnogo dvigatelya, realizuyushchego tsikl goreniya, priblizhennyy k detonatsionnomu [On the development of an air-jet engine implementing a combustion cycle close to the detonation cycle]. Goren. Vzryv (Mosk.) — Combustion and Explosion 14(1):29–37.
- Migalin, K. V., K. A. Sidenko, and K. K. Migalin. 2021. Ezhektornye dvukhkonturnye pul’siruyushchie vozdushno- reaktivnye dvigateli dlya okolo i sverkhzvukovykh skorostey poleta [Ejector double-circuit pulsejets for transonic and supersonic flight speeds]. Togliatti: Spectrum Publishing House. 121 p.
- Knysh, Yu. A., and A. F. Uryvskiy. 1984. Model of swirled jet vortical core precession. Soviet Aeronautics 27(3):48–50.
- Gupta, A. K., D.G. Lilley, and N. Syred. 1984. Swirl flows. Turnbridge Wells, England: Abacus Press. 488 p.
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