Investigation of the Development of Unsteady Flow Separation from a Model Swept Wing

I. V. Kolin; V. G. Markov; V. L. Sukhanov; T. I. Trifonova; D. V. Shukhovtsov

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Investigation of the Development of Unsteady Flow Separation from a Model Swept Wing

机译：模型后掠翼非定常流动分离的发展研究

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摘要

The results of an experimental wind-tunnel investigation of the flow patterns on the swept wing of a model aircraft realized for pitching oscillations with an amplitude A_α = 5° with respect to setup angles of attack α_0 = 10 and 16° are presented.

机译：给出了对模型飞机后掠机翼上的流型进行风洞实验研究的结果，该模型实现了相对于攻角α_0= 10和16°俯仰幅度为A_α= 5°的振荡。

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来源
《Fluid Dynamics》 |2009年第5期|共7页
作者
I. V. Kolin; V. G. Markov; V. L. Sukhanov; T. I. Trifonova; D. V. Shukhovtsov;
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原文格式 PDF
正文语种 eng
中图分类流体力学;
关键词
Flow separation; Unsteady flows; Swept wing; Oscillation frequency; Boundary layer; Viscous-inviscid interaction; Angle of attack; Angle of yaw;

机译：流动分离;非恒定流动;后掠翼;振荡频率;边界层;粘稠相互作用;攻角;偏航角;

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专利

1. Investigation of the Development of Unsteady Flow Separation from a Model Swept Wing [J] . I. V. Kolin, V. G. Markov, V. L. Sukhanov, Fluid Dynamics . 2009,第5期

机译：模型后掠翼非定常流动分离的发展研究
2. A THEORETICAL INVESTIGATION OF THE DEVELOPMENT OF STATIONARY CROSSFLOW VORTICES IN THE BOUNDARY LAYER ON A SWEPT WING [J] . 罗纪生, 周恒力学学报：英文版 . 1998,第002期

机译：扫翼边界层静止交叉流动发展的理论研究
3. Experimental and theoretical study of swept-wing boundary-layer instabilities. Unsteady crossflow instability [J] . Borodulin V. I., Ivanov A. V., Kachanov Y. S., Physics of fluids . 2019,第6期

机译：扫翼边界层稳定性的实验与理论研究。不稳定的跨流量不稳定
4. Numerical Investigations of Flow Separation on the AVT-183 53-deg Swept Diamond Wing Configuration [C] . Derick T. Daniel, Donald J. Malloy, Daniel A. Reasor Jr., AIAA aerospace sciences meeting;AIAA SciTech Forum . 2015

机译：AVT-183 53度后掠金刚机翼结构流分离的数值研究
5. Experimental investigation of the three-dimensional unsteady flow over a pitching backward swept wing. [D] . Karim, Md. Ahsanul. 1997

机译：俯仰后掠机翼上三维非定常流动的实验研究。
6. Investigating the Three-dimensional Flow Separation Induced by a Model Vocal Fold Polyp [O] . Kelley C. Stewart, Byron D. Erath, Michael W. Plesniak 2014

机译：研究模型人声折叠息肉引起的三维流分离
7. Step Response of Unsteady Aerodynamics Acting on Plane Swept Wing in Incompressible Flow for Finite State Modeling. [O] . Shinji SUZUKI, Kosyu KADOTA 1991

机译：不稳定空气动力学作用在平面扫翼的不压态模型中的扫翅上的步骤响应。
8. LOW-SPEED INVESTIGATION OF A FULL-SPAN INTERNAL-FLOW JET-AUGMENTED FLAP ON A HIGH-WING MODEL WITH A 35° SWEPT WING OF ASPECT RATIO 7.0 [R] . Thomas R. Turner 1960

机译：高宽度模型中具有35°sWEpT宽幅比的全跨内部流动射流增强的低速研究

Investigation of the Development of Unsteady Flow Separation from a Model Swept Wing

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