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A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution

机译：一种设计具有所需厚度分布的涡轮机叶片的方法，用于沿着任意的旋转细丝流动的可压缩流动

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Wu, Chung-Hua; Brown, Curtis A;
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年度 1951
页码 1-46
总页数 46
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Comparison of turbulence methods in CFD analysis of compressible flows in radial turbomachines [J] . R. Aghaei tog A.M. Tousi A. Tourani Aircraft Engineering and Aerospace Technology . 2008,第6期

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2. An Improved Mixing-Plane Method for Analyzing Steady Flow Through Multiple-Blade-Row Turbomachines [J] . Ding Xi Wang Journal of turbomachinery . 2014,第8期

机译：一种改进的混合平面方法，用于分析多叶片行涡轮机的稳定流动
3. Arbitrary Lagrangian-Eulerian methods for modeling high-speed compressible multimaterial flows [J] . Barlow Andrew J., Maire Pierre-Henri, Rider William J., Journal of Computational Physics . 2016,第Null期

机译：用于高速可压缩多材料流建模的任意拉格朗日-欧拉方法
4. On Uniqueness of Inverse Problem Solution of Compressible Flow Along an Arbitrary Stream Sheet of Revolution: (I) Channel Design [C] . Gao-Lian Liu International Symposium on Air Breathing Engines . 2007

机译：沿着任意流革命逆问题逆问题解决方案的独特性：（i）渠道设计
5. Three-dimensional inverse method for turbomachine blades by the circulation method: The thickness problem. [D] . Jiang, Jun. 1998

机译：涡轮机叶片的三维逆方法，循环法：厚度问题。
6. Cross-stream diffusion under pressure-driven flow in microchannels with arbitrary aspect ratios: a phase diagram study using a three-dimensional analytical model [O] . Hongjun Song, Yi Wang, Kapil Pant -1

机译：具有任意纵横比的微通道的压力驱动流下的交叉流扩散：使用三维分析模型的相图研究
7. A New Method of Calculating Optimum Velocity Distribution Along the Blade Surface on Arbitrary Stream Surface of Revolution in Turbomachines [O] . Zou Zixiang, Yuan Ding 1987

机译：一种在涡轮机中旋转旋转任意流表面上沿叶片表面计算最佳速度分布的新方法

A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution

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