Prediction method for spoiler performance
The prediction of the aerodynamic characteristics of a finite rectangular wing with part span spoilers is attempted using the lifting line theory of Prandtl. Required inputs to the theory are sectional values of lift coefficient, pitching moment coefficient, zero lift angle of attack, and aerodynami...
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| Language: | English |
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2010
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| Online Access: | http://hdl.handle.net/2429/20783 |