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An analysis method for the viscous/inviscid flow around airfoils with extensive trailing edge separation including surface roughness effects.

机译：具有广泛后缘分离的粘液/抗粘性流动的分析方法，包括表面粗糙度效应。

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Sean Bittle;
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1. Spectral Analysis of Unsteady Shear Flows over a Rounded-Trailing-Edge Airfoil [J] . Itsariyapinyo Pititat, Sharma Rajnish N. Journal of Aircraft . 2019,第1期

机译：圆弧形后缘翼型上非定常剪切流的频谱分析
2. Improved roughness model for turbulent flow in 2D viscous-inviscid panel methods [J] . Olsen Anders Smaerup, Ramos-Garcia Nestor, Bak Christian Wind Energy . 2020,第3期

机译：二维粘性-无粘性面板方法中湍流的改进粗糙度模型
3. Viscous-inviscid method for the simulation of turbulent unsteady wind turbine airfoil flow [J] . L. Bermudez, A. Velazquez, A. Matesanz Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2002,第6期

机译：粘性非粘性方法模拟风轮机非定常湍流
4. Comparison of Viscous and Inviscid Loads in a Static Aeroelastic Model of the Variable Camber Continuous Trailing Edge Flap Concept in the Transonic Regime [C] . M. Denison, J.A. Housman, E. Ting, AIAA applied aerodynamics conference;AIAA aviation forum . 2016

机译：跨音速状态下可变凸面连续后缘襟翼概念的静态气动弹性模型中粘性和无粘性载荷的比较
5. High-resolution TVD schemes for the analysis of: I. Inviscid supersonic and transonic flows. II. Viscous flows with shock-induced separation and heat transfer. [D] . Driver, Mark Anthony. 1991

机译：用于分析以下内容的高分辨率TVD方案：I.超音速和跨音速无粘性流。二。粘性流具有激振引起的分离和热传递。
6. Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique [O] . Gholamhossein Taherian, Mahdi Nili-Ahmadabadi, Mohammad Hassan Karimi, -1

机译：使用PIV技术以低雷诺数在具有基本空腔的厚钝尾缘翼型上进行流动可视化
7. Development of a Computer-Code for Viscous-Inviscid Analysis of Transonic Flow past Airfoils and Wings including Shock-wave Boundary Layer Interactions - Closure Report for ARDB project AE-O-147 [O] . Nandanan M, Shantha Kumari S 1987

机译：开发用于机翼和机翼的跨音速粘性流-粘性分析的计算机代码，包括冲击波边界层相互作用-ARDB项目AE-O-147的结案报告
8. A Potential-Flow/Boundary-Layer Method for Calculating Subsonic and Transonic Airfoil Flow with Trailing-Edge Separation [R] . Barnwell, R. W. 1981

机译：利用后缘分离计算亚音速和跨音速翼型流动的势流/边界层法

An analysis method for the viscous/inviscid flow around airfoils with extensive trailing edge separation including surface roughness effects.

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