A multi-disciplinary conceptual design methodology for assessing control authority on a hybrid wing body configuration
The primary research objective was to develop a methodology to support conceptual design of the Hybrid Wing Body (HWB) configuration. The absence of a horizontal tail imposes new stability and control requirements on the planform, and therefore requiring greater emphasis on control authority assess...
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| Format: | Others |
| Language: | en_US |
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Georgia Institute of Technology
2016
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| Online Access: | http://hdl.handle.net/1853/54328 |