振動する円柱の境界層の実験

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タイトル別名
  • Experiments on the Boundary Layer of an Oscillating Circular Cylinder
  • シンドウ スル エンチュウ ノ キョウカイソウ ノ ジッケン

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The mean and fluctuating velocities in the boundary layer of a circular cylinder, oscillating in the direction of the wind tunnel stream, have been measured using the hot-wire anemometer. The results have been compared with theoretical predictions. (1) The effect of the volocity fluctuation on the mean velocity in the boundary layer is found to be negligible when the ratio of the amplitude of fluctuation of the outer flow to the mean velocity is less than 0.3. This agrees with theoretical predictions. (2) Upsteam from the point of minimum pressure, the effect of the frequency of oscillation on the boundary layer is found to be negligible when the frequeney parameter is less than 0.3. The results of calculation, on the assumption of quasisteady flows, agree well with experimental velocity distributions. (3) When the separation point is approached, the discrepancy between the theoretical and experimental results increases. Although the discrepancy is mainly attributable to the premature truncation of the series solution used in the theoretical calculation, other causes are left to be explored.

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