Chinese
您当前的位置：
首页 >
文章列表页 >
Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion
更新时间：2026-07-07

    • Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion

    • Vol. 25, Issue 9, (2010)

    • Published：2010

    移动端阅览

  • XIAO Bao-guo, YANG Shun-hua, ZHAO Hui-yong, et al. Detailed and reduced chemical kinetic mechanisms for RP-3 aviation kerosene combustion[J]. 2010, 25(9). DOI：

  •  
  •  
icon
试读结束，您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束，您可以通过登录账户，到个人中心，购买VIP会员阅读全文。
已是VIP会员？
去登录 >

0

Views

765

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Application of reduced chemical kinetic model for ethylene combustion in combustor calculation of HIFiRE
Numerical simulations of flow field of rotating detonation engine fueled by kerosene
Effect of key parameters on knock of two⁃stroke kerosene engine
Effect of lean blowout performance of trapped vortex combustor of the afterburner
Research on mixture formation of two⁃stroke heavy fuel direct injection engine

Related Author

XIAO Bao-guo
ZHAO Hui-yong
YANG Shun-hua
XING Jian-wen
Fan YANG
Yuhui WANG
Shiquan LI
Guoqing ZHANG

Related Institution

Science and Technology on Scramjet Laboratory, Hypersonic Aerodynamics Research Institute, China Aerodynamics Research and Development Center
College of Mechanical and Electrical Engineering，Beijing University of Chemical Technology
School of Aerospace Engineering，Beijing Institute of Technology
College of Energy and Power Engineering，Nanjing University of Aeronautics and Astronautics
Sichuan Gas Turbine Establishment，Aero Engine Corporation of China
0