Perforated rudder for inhibiting vortex excitation vibration and design method thereof

All-through pressure holes are formed in the tail edge of a rudder wing in the flow direction and the spanwise direction, a pressure surface and a suction surface are communicated, and the tapping principle is as follows: a) a tapping area is in front of the tail edge and behind 3/4 of the chord len...

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Bibliographische Detailangaben

Hauptverfasser:	WANG ZHAOYU, YANG YUNONG, WANG CHUNXU, WANG QING, XIONG JISHI, DAI JINCHI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT CARRIERS EQUIPMENT FOR SHIPPING MINE-LAYING MINE-SWEEPING OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS PERFORMING OPERATIONS RELATED EQUIPMENT SHIPS OR OTHER WATERBORNE VESSELS SUBMARINES TRANSPORTING
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