スーパキャビテーション翼形の定常・非定常特性とねじりフラッタ限界

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タイトル別名
  • Supercavitation Hydrofoil Performance and Torsional Flutter Margin.
  • スーパキャビテーション ヨクケイ ノ テイジョウ ヒテイジョウ トクセイ ト ネジリ フラッタ ゲンカイ

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Supercavitation hydrofoil applied to high-speed marine propeller or hydro-machinery blade runs into unsteady behaviors such as cavitation breakdown and hydraulic flutter in some operation range. The hydrofoil performance was experimentally estimated and compared with the wedge performance using the cavitation tunnel and the torsional vibration apparatus with three component load cells. This experiment was carried out at several angles of attack in the region from subcavitation to supercavitation. At a general steady state but including some cavitation breakdowns, the hydrofoil has the most superior time mean lift/drag ratio about 6<Cl/Cd<8 at in all cavitation regions. But, the ratio drastically decreases as the angle of attack increases. Fluctuating lift coefficient C'l due to the cavitation breakdown reaches up to about 10% of time mean lift coefficient Cl. At the hydrofoil pitching motion, the torsional flutter margin of the hydrofoil extends to higher reduced frequency side as the angle of attack increases and has the nearly same margin of the wedge in all cavitation regions.

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