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RAPID ESTIMATION OF N-FACTORS FOR TRANSITION PREDICTION

机译:过渡预测的N因子快速估算

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Accurate prediction of transition from laminar to turbulent flow is not only needed for drag estimation, but is also important in predicting scale effects when extrapolating wind tunnel data to full scale. One of the methods commonly used for estimating the most likely position of this transition is based on stability theory. Linear stability theory is used to calculate the spatial evolution of all possible instability waves. If any wave exceeds some maximum amplification the ensuing nonlinear behaviour is assumed to cause a rapid breakdown to turbulence. From a correlation of calculated amplification factors with a large amount of experimental data a value of critical amplification has been found to be roughly e~n, where n is 9. This so called "e-to-n" approach has been used for many years and although not precise it is still one of the best tools available for the purpose of estimating the location of transition. The process of calculating all the eigensolutions needed, especially in three-dimensional boundary layers, can be quite time consuming and the estimation of the transition turns out to be too expensive for routine design purposes. Here we demonstrate an approximate way of calculating eigensolutions that can be used to speed up the prediction process significantly. Approximate eigenvalues are obtained from a set of pre-computed tables covering the required range of pressure gradients, Reynolds numbers and frequencies.
机译:准确估算从层流到湍流的转变不仅是阻力估算的必要条件,而且在将风洞数据外推到满比例时,在预测比例效应方面也很重要。通常用于估计此过渡的最可能位置的方法之一是基于稳定性理论。线性稳定性理论用于计算所有可能的不稳定波的空间演化。如果任何波超过某个最大放大倍数,则认为随之而来的非线性行为会导致湍流迅速击穿。从计算出的放大因子与大量实验数据的相关性,已发现临界放大倍数的值大致为e〜n,其中n为9。这种所谓的“ e-n”方法已被用于许多领域。多年,尽管不够精确,但它仍然是估算过渡位置的最佳工具之一。计算所需的所有本征解的过程(尤其是在三维边界层中)可能会非常耗时,并且转换的估计结果对于常规设计而言过于昂贵。在这里,我们演示了一种计算本征解的近似方法,该方法可用于显着加快预测过程。近似特征值是从一组预先计算的表中获得的,这些表涵盖了所需的压力梯度范围,雷诺数和频率。

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