Zobrazeno 1 - 10
of 314
pro vyhledávání: '"combusters"'
Autor:
Andreas Rees, Michael Oschwald
Publikováno v:
Fluid Mechanics and Its Applications ISBN: 9783031090073
The substitution of the toxic hydrazine in current high-altitude rocket engines like upper stages or reaction control thrusters by green propellants is a major key driver in the current technology development of rocket propulsion systems. Operating t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd4a3b39e82f9ead0535c499489c787d
https://doi.org/10.1007/978-3-031-09008-0_11
https://doi.org/10.1007/978-3-031-09008-0_11
Kniha
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Autor:
Andreas Rees, Michael Oschwald
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1240:012103
Due to current and future environmental and safety issues in space propulsion, typical propellants for upper stage or satellite rocket engines such as the toxic hydrazine are going to be replaced by green propellants like the combination of liquid ox
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::425beec2ef414e3a196188c5454075f7
https://doi.org/10.1088/1757-899x/1240/1/012103
https://doi.org/10.1088/1757-899x/1240/1/012103
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Publikováno v:
Chemosphere. 24:271-280
Using a database of nearly 500 documents, this study presents a comparison of levels of metals in municipal solid waste, the ash produced after incinerating the refuse, and the soils in which the ash is landfilled. The data are extremely variable.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0567554f4897684bbf40201565b4d0e8
https://doi.org/10.1016/0045-6535(92)90296-4
https://doi.org/10.1016/0045-6535(92)90296-4
Autor:
Ephraim Gutmark
Detailed measurements of velocity statistics, temperature distribution, flame chemiluminescence, and emission characteristics in a lean direct fuel injection multi swirl gas turbine combustor were acquired. The inlet and exit boundary conditions, inc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f12fa30a2329c8fd0a9bec0afc66ef0a
https://doi.org/10.21236/ada463219
https://doi.org/10.21236/ada463219
Autor:
Rees, Andreas, Oschwald, Michael
Publikováno v:
IOP Conference Series: Materials Science and Engineering; May 2022, Vol. 1240 Issue: 1 p012103-012103, 1p
Autor:
Masaya Umemoto, Goro Masuya, Yoshihiko Zamma, Sadatake Tomioka, Hironori Kitadani, Muneo Izumikawa
Publikováno v:
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The pre-ignition phase flow-field in a supersonic combustor with perpendicular injectors behind a backward-facing step was simulated with cold airflow and inert gas injection. The effects of injector configuration on pressure and injectant concentrat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0c44231d532998a622cfcc3cdbb22c38
https://doi.org/10.2514/6.1998-3127
https://doi.org/10.2514/6.1998-3127