## Abstract The aerodynamic force and flow structure of a wing performing an unsteady motion at small Reynolds number (__Re__=4000) is calculated by solving NavierβStokes equations. Calculations were conducted for steady motion, simple unsteady motions suc as azimuth rotation, pure translation, fea
THE LIFT GENERATED BY VIBRATIONAL MOTIONS
β Scribed by D.-C. LIU
- Publisher
- Elsevier Science
- Year
- 2001
- Tongue
- English
- Weight
- 232 KB
- Volume
- 245
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
By applying the reacted pressure on the &&deformed'' surface, we have calculated theoretically the time-averaged lift forces exerted on a vibrating body in the #uid medium with the non-viscosity and small disturbance assumptions. The lift turns out to be proportional to the product of the amplitudes of translating and deforming vibrations. We could thus deduce the scaling law applicable for the forces generated by the vibrational motions in the #uid medium.
2001 Academic Press
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