Publication:
Air-breathing pulsed detonation thrust module: Numerical simulations and firing tests

Простая страница элемента
dc.contributor.authorZangiev, A. E.
dc.contributor.authorFrolov, S. M.
dc.contributor.authorAksenov, V. S.
dc.contributor.authorIvanov, V. S.
dc.contributor.authorShamshin, I. O.
dc.contributor.authorФролов, Сергей Михайлович
dc.contributor.authorАксенов, Виктор Серафимович
dc.date.accessioned2024-11-20T10:59:17Z
dc.date.available2024-11-20T10:59:17Z
dc.date.issued2019
dc.description.abstract© 2019 Elsevier Masson SAS The air-breathing pulsed detonation thrust module (TM) for an aircraft designed for a subsonic flight at a speed of up to 120 m/s when operating on a standard aviation kerosene was developed using the analytical estimates and parametric multivariant three-dimensional (3D) calculations. The TM consists of an air intake with a check valve, a fuel supply system, a prechamber-jet ignition system and a combustion chamber with an attached detonation tube. An experimental sample of TM was fabricated, and its firing tests were carried out on a test rig with a thrust-measuring table. In firing tests, TM characteristics are obtained in the form of dependencies of effective thrust, aerodynamic drag and fuel-based specific impulse on fuel consumption at different speeds of the approaching air flow. It has been experimentally shown that the fuel-based specific impulse of the TM reaches 1000-1200 s, and the effective thrust developed by it reaches 180–200 N.
dc.format.extentС. 275-287
dc.identifier.citationAir-breathing pulsed detonation thrust module: Numerical simulations and firing tests / Zangiev, A.E. [et al.] // Aerospace Science and Technology. - 2019. - 89. - P. 275-287. - 10.1016/j.ast.2019.04.005
dc.identifier.doi10.1016/j.ast.2019.04.005
dc.identifier.urihttps://www.doi.org/10.1016/j.ast.2019.04.005
dc.identifier.urihttps://www.scopus.com/record/display.uri?eid=2-s2.0-85064265736&origin=resultslist
dc.identifier.urihttp://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=Alerting&SrcApp=Alerting&DestApp=WOS_CPL&DestLinkType=FullRecord&UT=WOS:000469896800023
dc.identifier.urihttps://openrepository.mephi.ru/handle/123456789/16871
dc.relation.ispartofAerospace Science and Technology
dc.titleAir-breathing pulsed detonation thrust module: Numerical simulations and firing tests
dc.typeArticle
dspace.entity.typePublication
oaire.citation.volume89
relation.isAuthorOfPublicationf1496521-237e-4526-bfeb-2206034d980e
relation.isAuthorOfPublication6dba94bf-de3b-4212-a139-9edab265d3af
relation.isAuthorOfPublication.latestForDiscoveryf1496521-237e-4526-bfeb-2206034d980e
relation.isOrgUnitOfPublicationdcdb137c-0528-46a5-841b-780227a67cce
relation.isOrgUnitOfPublication.latestForDiscoverydcdb137c-0528-46a5-841b-780227a67cce
Файлы
Коллекции
Публикации