training and arrangement of zulaufringes or ablaufsammelringes for schubduesen or combustion chambers of raketentriebwerken, especially fluessigkeitsraketentriebwerken

• 1. 一种液体火箭发动机推力室身部的集液环 [P] . 中国专利： CN208885408U . 2019.05.21
• 2. 一种液体火箭发动机推力室身部的集液环 [P] . 中国专利： CN108979900A . 2018-12-11
• 3. training and arrangement of zulaufringes or ablaufsammelringes for schubduesen or combustion chambers of raketentriebwerken, especially fluessigkeitsraketentriebwerken [P] . 法国专利： FR2006438A1 . 1969-12-26

  机译： 火箭发动机，尤其是液体火箭发动机的推力喷嘴或燃烧室的进气环或排水收集器环的培训和布置

• 4. combustion chamber with schubdruese of fluessigkeitsraketentriebwerken [P] . 法国专利： FR2041104B2 . 1974-08-09

  机译： 液体火箭发动机带推力阀的燃烧室

• 5. device for assigning a zuendmittels for combustion chambers of fluessigkeitsraketentriebwerken [P] . 德国专利： DE000001626050A . 1971-06-24

  机译： 为fluessigkeitsraketentriebwerken燃烧室分配zuendmittels的设备

• 1. Numerical simulation of plasma-assisted combustion of methane-air mixtures in combustion chamber [J] . Jun DENG, Liming HE, Xingjian LIU, 等离子体科学和技术（英文版） . 2018,第012期
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• 3. Three-dimensional Numerical Simulation of Combustion Field in the Combustion Chamber [J] . YAN Ping, QIAN Zhi-bo, YANG Jie, 兵工学报（英文版） . 2006,第002期
• 4. Optimal arrangement for pressure measurement points in working chamber of earth pressure balance shield [J] . LIU Chang, QU Fu-zheng, LI Shou-ju, 中南大学学报（英文版） . 2012,第007期
• 5. LINEAR REACTIVE ENGINE WITH ACTIVE CONTROL OF A CRITICAL SECTION AND WITH A MULTI-TIERED ARRANGEMENT OF COMBUSTION CHAMBERS [C] . Oleg Aleksandrov International astronautical congress . 2014
• 6. Design and Analysis of a Constant Volume Combustion Chamber to Test Premixed Combustion [D] . Nonavinakere Vinod, Kaushik 2018
• 7. Data on combustion chamber measurements of a diesel engine fuelled with biodiesel of jatropha curcas and fatty acid distillates [O] . Ramón Piloto-Rodríguez, Marianela Ortiz-Alvarez, Jesús Suárez-Hernández, 2020
• 8. Studies on the Combustion of the Precombustion Chamber Diesel Engine : 4th Report, The Effect of Fuel Characteristics Fuel Injection Rate, and Precombustion Chamber Shapes on the Combustion [O] . Seok Hong SEO, Tong Ku KIM 1967
• 9. ALTITUDE-TEST-CHAMBER INVESTIGATION OF PERFORMANCE OF A 28-INCH RAM-JET ENGINE Ⅳ – EFFECT OF INLET-AIR TEMPERATURE, COMBUSTION-CHAMBER-INLET-MACH NUMBER, AND FUEL VOLATILITY ON COMBUSTION PERFORMANCE [R] . Robert W. Kahn, Shigeo Nakanishi, James L.Harp 1951

• 1. Optimal arrangement for pressure measurement points in working chamber of earth pressure balance shield [J] . 刘畅 ,屈福政 ,李守巨 . 中南大学学报 . 2012,第007期
• 2. 小推力液体火箭发动机燃烧室脉冲工作过程简化分析 [C] . 唐振宇 ,侯凤龙 ,何小英 . 2009年中国宇航学会学术年会 . 2009
• 3. 液体火箭发动机燃烧室内两相流动特性的数值分析 [A] . 刘国栋 . 2006