Aerodynamic properties of a wing performing unsteady rotational motions at low Reynolds number
β Scribed by S. L. Lan; M. Sun
- Publisher
- Springer Vienna
- Year
- 2001
- Tongue
- English
- Weight
- 723 KB
- Volume
- 149
- Category
- Article
- ISSN
- 0001-5970
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π SIMILAR VOLUMES
## 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
## Abstract This paper treats the kernel function of an integral equation that relates a known or prescribed upwash distribution to an unknown lift distribution for a finite wing. The pressure kernel functions of the singular integral equation are summarized for all speed range in the Laplace trans