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Efficiency and accuracy of time-accurate turbulent navier-stokes computations

机译:时间精确的湍流纳斯托克斯计算的效率和准确性

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The accuracy and efficiency of two types of subiterations in both explicit and implicit Navier-Stokes codes are explored for unsteady laminar circular-cylinder flow and unsteady turbulent flow over an 18-percent-thick circular-arc (biconvex) airfoil. Grid and time-step studies are used to assess the numerical accuracy of the methods. Nonsubiterative time-stepping scheems and schemes with physical time subiterations are subject to time-step limitations in practice that are removed by pseudo time subiterations. Computations for the circular-arc airfoil indicate that a one-equation turbulence model predicts the unsteady separated flow better than an algebraci turbuelnce model; also the hysteresis with Mach number of the self-excited unsteadiness due to shock and boundary-layer separation is well predicted.
机译:研究了显式和隐式Navier-Stokes代码中两种子迭代的准确性和效率,以研究18%厚的圆弧(双凸面)机翼上的非恒定层流圆柱流和非恒定湍流。网格和时间步研究用于评估方法的数值准确性。具有物理时间子迭代的非替代性时间步调方案和方案在实践中会受到时间步长的限制,这些限制可以通过伪时间子迭代来消除。对圆弧翼型的计算表明,单方程湍流模型比代数湍流模型更好地预测了非定常分离流。还可以很好地预测由于冲击和边界层分离而引起的自激非稳态马赫数滞后现象。

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