Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines [0.03%]
吸气式发动机进气口和喷嘴的集成设计与分析
Ferlauto, M.; Larocca, F.; Zannetti et al.
Ferlauto et al.
Effects of Orifice Geometry on Gelled Propellants Sprayed from Impinging-Jet Injectors [0.03%]
孔口几何形状对冲击射流喷射器喷射胶凝推进剂的影响
Fu, Qing-fei; Yang, Li-jun; Cui et al.
Fu et al.
Schoenitz, Mirko; Dreizin, Edward L.
Schoenitz
Martinez-Sanchez, Manuel; Miller, Scott A.
Martinez-Sanchez
Burning Rate of Solid Propellant Ingredients, Part 2: Determination of Burning Rate Temperature Sensitivity [0.03%]
固体推进剂成分的燃烧速率，第2部分：燃烧速率温度灵敏度的测定
Atwood, A. I.; Boggs, T. L.; Curran et al.
Atwood et al.
Combustion Stability Analysis of Rocket Engines with Resonators Based on Nyquist Plots [0.03%]
基于奈奎斯特图的带谐振腔火箭发动机燃烧稳定性分析
Cárdenas-Miranda, A.; Polifke, W.
Cárdenas-Miranda
Wall Temperature Effects on Heat Transfer Coefficient for High-Pressure Turbines [0.03%]
壁温对高压汽轮机传热系数的影响
Maffulli, R.; He, L.
Maffulli
Harris, Paul Glendon; Ripley, Robert; Guzik et al.
Harris et al.