Zobrazeno 1 - 10
of 249
pro vyhledávání: '"Pressure gain combustion"'
Publikováno v:
INCAS Bulletin, Vol 16, Iss 3, Pp 67-75 (2024)
In order to obtain important knowledge for raising the performance and efficiency of propulsion systems, in this paper we investigate the dynamics process of pressure gain combustion in the Pulse Detonation Engine. Through comprehensive experimentati
Externí odkaz:
https://doaj.org/article/9a6cc6351f2b4af0964e115e5a61ebb4
Publikováno v:
Applications in Energy and Combustion Science, Vol 21, Iss , Pp 100313- (2025)
Rotating Detonation Engines (RDEs) are a form of pressure gain combustion (PGC), offering a promising approach to increase the thermodynamic efficiency of a gas turbine combustor by utilizing a detonation-driven combustion process. In most RDEs, fuel
Externí odkaz:
https://doaj.org/article/52e984b4b6694c48a64bb4711296c423
Autor:
Raj, Piyush
Pressure Gain Combustion (PGC) systems have gained significant focus in recent years due to its potential for increased thermodynamic efficiency over a constant pressure cycle (or Brayton cycle). A rotating detonation combustor (RDC) is a type of PGC
Externí odkaz:
https://hdl.handle.net/10919/120587
Publikováno v:
Applications in Energy and Combustion Science, Vol 19, Iss , Pp 100282- (2024)
Rotating detonation rocket engines are propulsive devices employing detonation waves moving circumferentially around an annular channel that consume axially fed propellants. Theoretically, this provides benefits with respect to combustion pressure ga
Externí odkaz:
https://doaj.org/article/5eae51e875de4b09b5c54c29abaa5bad
Publikováno v:
Frontiers in Aerospace Engineering, Vol 2 (2024)
Externí odkaz:
https://doaj.org/article/4cd8ae9e3aba494799a8133e9bb968c9
Autor:
Alina Bogoi, Tudor Cuciuc, Andrei Vlad Cojocea, Mihnea Gall, Ionuț Porumbel, Constantin Eusebiu Hrițcu
Publikováno v:
Aerospace, Vol 11, Iss 6, p 465 (2024)
A pulsed detonation chamber (PDC) equipped with Hartmann–Sprenger resonators has been designed and tested for both Hydrogen/air and Hydrogen/Oxygen mixtures. A full-factorial experimental campaign employing four factors with four levels each has be
Externí odkaz:
https://doaj.org/article/1690b88c2573426d8237e58d96e80216
Autor:
Sergio Grasa, Guillermo Paniagua
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 9, Iss 2, p 18 (2024)
In rotating detonation engines the turbine inlet conditions may be transonic with unprecedented unsteady fluctuations. To ensure an acceptable engine performance, the turbine passages must be suited to these conditions. This article focuses on design
Externí odkaz:
https://doaj.org/article/52457f485c92486a8f4dd0af3e2716d0
Publikováno v:
Energies, Vol 17, Iss 5, p 1191 (2024)
Pressure gain combustion cycles are under the spotlight due to their higher theoretical cycle thermal efficiency compared to conventional machines. Under this prism, a constant-volume combustor (CVC) prototype supplied with a mixture of air and liqui
Externí odkaz:
https://doaj.org/article/3183c1f653f349ab8866bebe03bb9dbd
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Akademický článek
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