Distribution of aerofoil section lift from section pitching moment applied to a dynamic model for aircraft poststall departure
A method for chordwise redistribution of lift over a wing for poststall flight simulation is investigated. Aerofoil section moment data is used to divide and distribute into two parts the wing lifting line of Prandtl finite wing circulation theory. The method of lift distribution is applied in the a...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/41084 http://scholar.lib.vt.edu/theses/available/etd-02132009-172236/ |