Unsteady flow through a cascade of aerofoils

A. H. Low

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Unsteady flow through a cascade of aerofoils

机译：不稳定的流过一系列翼型

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SummaryThis paper extends some earlier work by Woods [8] on the transient forces caused by unsteady transverse motions of a rigid cascade of aerofoils to the case when the inlet velocity is varying in magnitude. The flow is incompressible and two-dimensional. Expressions for the growth of lift and moment on a member of the cascade with increasing inlet velocity are evaluated and shown to be generalizations of Wagner's classical results for an isolated aerofoil.

机译：结束语本文将伍兹[8]的一些早期工作扩展到了由刚性翼型叶栅的不平稳横向运动引起的瞬态力到进口速度大小变化的情况下。流是不可压缩的并且是二维的。评估了随着进气速度的增加，叶栅上的升力和力矩的增长表达式，并被证明是Wagner对孤立翼型经典结果的推广。

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《Journal of the Australian Mathematical Society》 |2009年第2期|共页
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A. H. Low;
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1. Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding [J] . Kiran Ramesh, Ashok Gopalarathnam, Kenneth Granlund, Journal of Fluid Mechanics . 2014,第Null期

机译：具有新颖脱落准则的离散涡旋方法，用于不定常翼型流动且具有间歇性前沿涡旋脱落
2. Organised modes and shock-vortex interaction in unsteady viscous transonic flows around an aerofoil - Part II: Reynolds number effect [J] . A. Bouhadji, M. Braza Computers & Fluids . 2003,第9期

机译：机翼周围非稳定粘性跨音速流动中的有组织模式和激涡相互作用-第二部分：雷诺数效应
3. Organised modes and shock-vortex interaction in unsteady viscous transonic flows around an aerofoil - Part I: mach number effect [J] . A. Bouhadji, M. Braza Computers & Fluids . 2003,第9期

机译：翼型周围非稳定粘性跨音速流动中的组织模式和激涡相互作用-第一部分：马赫数效应
4. Numerical Simulation of Unsteady Aerodynamic Loads over an Aerofoil in Transonic Flow [C] . Yu Qian, JunLi Yang, XiaoJun Xiang, MEE 2012 . 2013

机译：在跨音速流动中不稳定空气动力载荷的数值模拟
5. Unsteady flows in a two-dimensional linear cascade with low-pressure turbine blades. [D] . Murawski, Christopher Gabriel. 1999

机译：带有低压涡轮叶片的二维线性叶栅中的非稳态流动。
6. Potential flow through a cascade of aerofoils: direct and inverse problems [O] . P. J. Baddoo, L. J. Ayton -1

机译：流经一系列翼面的势能：正向和反向问题
7. Unsteady Characteristics of the Oscillating Aerofoils of Arbitrary Section in Cascade : 3rd Report, Aerofoil Section of Large Camber and Thickness [O] . Tetsuo NISHIYAMA, Minoru MURATA 1978

机译：级联任意部分振荡翼型的不稳定特性：第三次报告，大型弯曲和厚度的机翼段
8. The Two-dimensional Subsonic Flow of an Inviscid Fluid about an Aerofoil of Arbitrary Shape Part I. Incompressible Flow about a Symmetrical Aerofoil in a Channel or Free Stream. Part II. Incompressible Flow about an Asymmetric Aerofoil in a Free Stream. Part III. The Influence Factor Method of Calculating Incompressible Flow. Part IV. Compressible Flow. [R] . L. C. WOODS 1953

机译：关于任意形状翼型的Inviscid流体的二维亚音速流动。关于通道或自由流中对称翼型的不可压缩流动。第二部分。关于自由流中不对称翼型的不可压缩流动。第三部分。计算不可压缩流动的影响因素法。第四部分。可压缩流动。

Unsteady flow through a cascade of aerofoils

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