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Modern Adaptation of Prandtl's Classic Lifting-Line Theory

✍ Scribed by Phillips, W. F.; Snyder, D. O.


Book ID
125487217
Publisher
American Institute of Aeronautics and Astronautics
Year
2000
Tongue
English
Weight
391 KB
Volume
37
Category
Article
ISSN
0021-8669

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πŸ“œ SIMILAR VOLUMES


On an extension of Prandti's lifting lin
✍ S. PrΓΆssdorf; D. Tordella πŸ“‚ Article πŸ“… 1991 πŸ› Elsevier Science βš– 992 KB

In this paper we propose an extension of Prandtl's lifting line theory to curved wings. The aim is to evidence the effect of the curved geometry on the aerodynamic efficiency. By means of an analytical-numerical integration methodology, leading asymptotically to an exponential convergence, we show t

Predictions of unsteady hawt aerodynamic
✍ H. Dumitrescu; V. Cardoş πŸ“‚ Article πŸ“… 2001 πŸ› Elsevier Science 🌐 English βš– 1009 KB

A numerical engineering method for the prediction of unsteady wind turbine aerodynamics is presented. The formulation is based on lifting line theory and a semiempirical dynamic stall model of Leishman and Beddoes. The unsteady aerodynamic response of the blade aerodynamics to the sharp blade-pitch