CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS

机译：跨音速翼型和无限扫掠翼计算分析中的过渡折算值的收敛性

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The effect of intermittent re-calculation oftransition position is analysed using a low-orderVII platform coupled to an Orr-Sommerfeld-typestability analysis method. Transonic aerofoil andinfinite-swept wing flows were studied. Where thetransition mechanisms are weakly dependent onthe gross flow field characteristics, as few as tentransition updates may be required over a 1000-iteration CFD solution, if correctly timed.

机译：间歇性重新计算的效果使用低阶分析过渡位置 VII平台与Orr-Sommerfeld型耦合稳定性分析方法。跨音速翼型和研究了无限掠过的机翼流动。哪里过渡机制几乎不依赖于总流场特征，只有十个可能需要在1000- 迭代CFD解决方案（如果正确计时）。

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《Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences》|2014年|1-8|共8页
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C J Atkin;
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transition modelling; CFD;

机译：过渡建模; CFD;

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专利

1. Infinite Swept-Wing Navier-Stokes Computations with e~N Transition Prediction [J] . Hans W. Stock AIAA Journal . 2005,第6期

机译：具有e〜N转换预测的无限扫频Navier-Stokes计算
2. Transition prediction in infinite swept wings using Navier-Stokes computations and linear stability theory [J] . J.M.M. Sousa, L.M.G. Silva Computers & Structures . 2004,第17a19期

机译：使用Navier-Stokes计算和线性稳定性理论的无限后掠翼的过渡预测
3. Fully Three-Dimensional Transition Prediction on Swept Wings in Transonic Flows [J] . Marc Langlois, Christian Masson, Ion Paraschivoiu Journal of Aircraft . 1998,第2期

机译：跨音速流扫掠机翼的全三维过渡预测
4. CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS [C] . C J Atkin Congress of the International Council of the Aeronautical Sciences . 2014

机译：跨音质空间计算分析过程中计算过渡基因座的融合与无限扫翅膀
5. Transonic Flow Around Swept Wings: Revisiting Von Karman's Similarity Rule. [D] . Kirkman, Jeffrey J. 2016

机译：横掠机翼的跨音速流动：再探冯·卡曼的相似性规则。
6. Computational analysis of calculated physicochemical and ADMET properties of protein-protein interaction inhibitors [O] . David Lagorce, Dominique Douguet, Maria A. Miteva, -1

机译：蛋白质-蛋白质相互作用抑制剂的理化和ADMET性质的计算分析
7. Analysis of transitional separation bubbles on infinite swept wings [O] . Davis R. L., Carter J. E. 1986

机译：无限扫掠机翼上的过渡分离气泡分析
8. Langley Stability and Transition Analysis Code (LASTRAC) : LST, Linear and Nonlinear PSE for 2-D, Axisymmetric, and Infinite Swept Wing Boundary Layers [R] . Chang, C. L. 2003

机译：Langley稳定性和跃迁分析代码（LasTRaC）：用于二维，轴对称和无限扫描翼边界层的LsT，线性和非线性psE

CONVERGENCE OF CALCULATED TRANSITION LOCI DURING COMPUTATIONAL ANALYSIS OF TRANSONIC AEROFOILS AND INFINITE SWEPT WINGS

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