Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Hirata Kousuke"'
Publikováno v:
In Diamond & Related Materials 2011 20(8):1171-1178
Autor:
Yuasa, Saburo, Shiraishi, Noriko, Sakamoto, Masafumi, Sezaki, Chinatsu, Hirata, Kousuke, Sakurai, Takashi
Publikováno v:
日本航空宇宙学会論文集. 59(687):97-101
The characteristic velocity C^* is derived from the assumption of one-dimensional flow in a uniform pressure field, and is usually evaluated using a combustion chamber pressure measured on the chamber wall. In the swirling-oxidizer-flow-type hybrid r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::a7b630f7bceaef0062dc5608eb3ae11e
http://hdl.handle.net/10748/00010482
http://hdl.handle.net/10748/00010482
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In order to increase the fuel regression rate of hybrid rocket engine, the concave-convex surface grain was adopted for the swirling-oxidizer-flow-type hybrid rocket engine. Burning experiments were carried out by changing the convex width from 9 to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b8a29e05c8363d8d7bfdb90cfdcfb77
https://doi.org/10.2514/6.2012-4107
https://doi.org/10.2514/6.2012-4107
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In the swirling-oxidizer-flow-type hybrid rocket engine with front head injection, the local fuel regression rates at the leading edge of the grain were considerably larger than those in the real region. The regression rate behaviors in both regions
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f44d9e7c4ac5ab90f6471c52779c6837
https://doi.org/10.2514/6.2012-4106
https://doi.org/10.2514/6.2012-4106
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In order to increase the fuel regression rate, the paraffin fuel was used in the swirlingoxidizer-flow-type hybrid rocket engine. To improve the poor combustion efficiency when using the paraffin fuels, the engine was improved to have a shorter lengt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40d7bc5d9860e32c044f595947f1d351
https://doi.org/10.2514/6.2012-3904
https://doi.org/10.2514/6.2012-3904
Fuel Regression Rate Behavior for Various Fuels in Swirling-Oxidizer-Flow-Type Hybrid Rocket Engines
Publikováno v:
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In order to clarify the overall and local fuel regression rate behavior of hybrid combustion in swirling oxidizer flow, burning tests of the swirling-oxidizer-flow-type hybrid rocket engine were conducted using PP , PMMA and WAX fuel grains. The expe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::80906956142615a20c521c29b06eb1ea
https://doi.org/10.2514/6.2011-5677
https://doi.org/10.2514/6.2011-5677
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