後退翼3次元境界層の乱流遷移における表面微小粗さと音波に対する受容性

概要

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The effect of micron-sized roughness in the leading edge region on a swept wing boundary-layer transition is examined experimentally in detail. By applying sound waves from a loud speaker, sound receptivity to turbulent transition is also investigated. Results showed that such a minute roughness element (κ=45μm in height, 1mm in diameter, κ/δ=0.23) placed at χ=40mm resulted in early transition. In the case that no transition enhancement was observed in the presence of a single roughness element, early transition also occurred with sound excitation. Low frequency disturbance f_1 responded strongly to the sound frequency, in particular, to the direction of the sound waves. Critical spacing of roughness elements where the transition is amplified the most seems to exist in the range of λ/δ≒1.3. It is also noted that no enhancement of transition occurs when the roughness element is placed beyond 20% of the chord length.
社団法人日本機械学会の論文
1996-06-25