A theoretical investigation of a low-correction windtunnel wall configuration for airfoil testing
This thesis deals with anew approach to reduce wall corrections in high-lift airfoil testing, by employing symmetrically transversely slotted walls. The solid elements of the slotted wall are symmetrical airfoils at zero incidence, the spaces between the slats are nonuniform, increasing linearly tow...
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| Language: | English |
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2010
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| Online Access: | http://hdl.handle.net/2429/21535 |