A study of methods to increase the lift of supersonic airfoils at low speeds
This thesis presents a study of the problem of improving the lift characteristics of a supersonic wing at low speeds. Trailing edge split flaps, nose flaps , and boundary layer control were investigated singularly and together using the optimum configuration of each.
| Main Authors: | , |
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| Language: | en_US |
| Published: |
California Institute of Technology
2012
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| Online Access: | http://hdl.handle.net/10945/6572 |