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

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

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

The effect of intermittent re-calculation of transition position is analysed using a low-order VII platform coupled to an Orr-Sommerfeld-type stability analysis method. Transonic aerofoil and infinite-swept wing flows were studied. Where the transition mechanisms are weakly dependent on the gross flow field characteristics, as few as ten transition updates may be required over a 1000- iteration CFD solution, if correctly timed.

机译：使用耦合到ORR-SOMMERFELD型稳定性分析方法的低位VII平台分析间歇重新计算过渡位置的效果。研究了跨音质机身和无限扫过的翼流。如果过渡机制弱依赖于总体流场特征，则在1000迭代CFD解决方案中可能需要10个转换更新，如果正确定时。

著录项

来源
《Congress of the International Council of the Aeronautical Sciences》|2014年||共8页
会议地点
作者
C J Atkin;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空;
关键词
transition modelling; CFD;

机译：过渡建模;CFD;

相似文献

外文文献
中文文献
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;International Council of the Aeronautical Sciences . 2014

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
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

摘要

著录项

相似文献

相关主题

期刊订阅