Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Fan XJ(范学军)"'
Publikováno v:
21st AIAA International Space Planes and Hypersonics Technologies Conference.
To explore the combustion performance of non-rectangular type supersonic combustors, the flow and combustion characteristics in round and round-to-elliptic shape-transition (RdEST) supersonic combustors under the same configurations of flight Mach nu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::031d44691eea0544b8b91a2bca1b63b8
https://doi.org/10.2514/6.2017-2190
https://doi.org/10.2514/6.2017-2190
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In this paper, a numerical analysis coupling heat transfers of the combustor internal flow, the coolant flow and the strut wall is developed and applied for the optimization of strut cooling using aviation kerosene as coolant at flow conditions corre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e9b9aea63e926c4f91f0e90bf0508dd
https://doi.org/10.2514/6.2012-3926
https://doi.org/10.2514/6.2012-3926
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Characteristics of supersonic combustion by injecting kerosene vapor into a Mach 2.5 crossflow at various preheat temperatures and pressures were investigated experimentally. A two-stage heating system has been designed and tested, which can prepare
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5140f11c8c42c015cfe7e80de5b9b68e
https://doi.org/10.2514/6.2004-3485
https://doi.org/10.2514/6.2004-3485