Hongxun, Chen; Haifeng, Li; Fajia et al.
Hongxun et al.
A Variation Finite Element Method for Solving the Blade-to-Blade Flow in Centrifugal Compressor's Cascades with Splitter Blades on an Arbitrary Streamsheet of Revolution and a Mathematical Treatment to the Region Behind Cascades [0.03%]
一种用于求解带有分流叶片的任意回转流面内离心压缩机叶栅中叶间流动的变分有限元方法，以及对叶栅后区域的数学处理
Yuelin, Chen; Zangmin, Chen; Daofang et al.
Yuelin et al.
Overall Performance Measurements of Annular Combusts Used in P-60 Miniature Turbojet Engine [0.03%]
P-60微型涡喷发动机所用环形燃烧室的综合性能测试
Tsai, Bor-Jang; Chang, Chung-Yen; Ho et al.
Tsai et al.
Effect of Tab Geometry on the Development of a Jet Issuing from a Rectangular Nozzle [0.03%]
矩形喷嘴射流发展的孔口几何形状影响
Arokkiaswamy, Abraham; Verma, Shashi Bhushan; Venkateswaran et al.
Arokkiaswamy et al.
Research for the Fluid Field of the Centrifugal Compressor Impeller in Accelerating Startup [0.03%]
离心压缩机叶轮加速启动过程中的流场研究
Li, Xiaozhu; Chen, Gang; Zhu et al.
Li et al.
Study on Practical Application of Turboprop Engine Condition Monitoring and Fault Diagnostic System Using Fuzzy-Neuro Algorithms [0.03%]
基于模糊神经算法的涡轮螺旋桨发动机状态监测与故障诊断系统实用化研究
Kong, Changduk; Lim, Semyeong; Kim et al.
Kong et al.
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor [0.03%]
入口边界层厚度对轴流压缩机损失特性的影响
Choi, Minsuk; Park, JunYoung; Baek et al.
Choi et al.
Rotaru, Constantin; Andres-Mihăilă, Mihai; Matei et al.
Rotaru et al.