Chiba, Noritane (2001) Behavior of Unsteady Cavity on a Wing Section. In: CAV 2001: Fourth International Symposium on Cavitation, June 20-23, 2001, California Institute of Technology, Pasadena, CA USA. (Unpublished) http://resolver.caltech.edu/CAV2001:sessionA8.006
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In order to simulate the cloud cavitation on hydraulic machinery, the unsteady cavitation on a rectangular wing section was observed in the cavitation channel of the Miyakonojo National College of Technology. The attack angle was forced to change from 10deg. to –10deg. by a strike of hammer. As the attack angle decreased, the sheet cavitation left the leading edge of wing and changed into cloud cavities on the mid-chord of wing.
|Item Type:||Conference or Workshop Item (Lecture)|
|Usage Policy:||The papers of this symposium proceedings are protected by copyright, retained by the authors. Authors control translation and reproduction rights to these works. However, readers are granted permission for individual, educational, research and non-commercial reproduction, distribution, display and performance of this work in any format. This permission is in addition to rights of reproduction granted under Section 107, 108, and other provisions of the U.S. Copyright Act.|
|Deposited By:||Imported from CAV2001|
|Deposited On:||01 May 2001|
|Last Modified:||26 Dec 2012 07:09|
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