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Method of Solving the Direct and Inverse Problem of Supersonic Flow Along Arbitrary Stream Filaments of Revolution in Turbomachines

机译：解决超音速的直接和反问题随着涡轮机中的革命的任意流丝的方法

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作者
Wu, C.; Costilow, E. L.;
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年度 1951
页码 1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Supersonic flow ; Two dimensional ; Filaments ; Supersonic nozzles ; Streams ; Turbomachinery ; Cascade structures ; Streamline shape;

机译：超音速流;二维;细丝;超音速喷嘴;流;透平机械;级联结构;流线形状;

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2. Application of a Direct Method for Solving the Boltzmann Equation in Supersonic Flow Computation [J] . Aristov V. V., Rovenskaya O. I. Computational mathematics and mathematical physics . 2016,第11期

机译：直接法求解玻尔兹曼方程在超声速计算中的应用
3. Application of a Direct Method for Solving the Boltzmann Equation in Supersonic Flow Computation [J] . Aristov V. V., Rovenskaya O. I. Computational mathematics and mathematical physics . 2016,第11期

机译：一种直接方法在超音流计算中求解Boltzmann方程的应用
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

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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. A novel self-seeding method for particle image velocimetry measurements of subsonic and supersonic flows [O] . Omid Nematollahi, Hadi Samsam-Khayani, Mahdi Nili-Ahmadabadi, -1

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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

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8. A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines [R] . Wu, Chung-Hua, Costilow, Eleanor L 1951

机译：一种求解涡轮机内任意流细丝的超音速流动的直接和反问题的方法

Method of Solving the Direct and Inverse Problem of Supersonic Flow Along Arbitrary Stream Filaments of Revolution in Turbomachines

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