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- OpenAccess
超音速燃燒衝壓引擎流場數值模擬
Numerical Simulation of Scramjet Engine
並列摘要
Scramjet engine is proper propulsion system for hypersonic fly in atmosphere. In this paper, a 2-D numerical program was builded successfully and a model engine operation performance analysis was accomplished. The result shows that bleeding system is an important link in inlet design and the boundary plays an important role in engine auto-ignition.
延伸閱讀
- 鄭伃均（2016）。超音速燃燒衝壓引擎燃燒室加入多孔性圓柱燃燒器之模擬與分析〔碩士論文，國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU201603446
- 林建宏（2009）。超音速燃燒衝壓引擎流場之直接模擬蒙地卡羅法模擬探討〔碩士論文，淡江大學〕。華藝線上圖書館。https://doi.org/10.6846/TKU.2009.00770
- Wu, Y. C. (2018). 脈衝爆震引擎噴嘴流場之初步數值模擬 [master's thesis, Tamkang University]. Airiti Library. https://www.airitilibrary.com/Article/Detail?DocID=U0002-2108201810215700
- 蔡明霏（2014）。使用加權基本不震盪算則之超音速衝壓引擎流場模擬分析〔碩士論文，國立臺灣大學〕。華藝線上圖書館。https://doi.org/10.6342/NTU.2014.10731
- Fondelli, T., Andreini, A., Soghe, R. D., Facchini, B., & Cipolla, L. (2015). Numerical Simulation of Oil Jet Lubrication for High Speed Gears. International Journal of Aerospace Engineering, 2015(), 585-597. https://doi.org/10.1155/2015/752457