A distributed actuation array was installed on a blended-wing-body uninhabited aerial vehicle and tested in the 12-foot subsonic wind tunnel at NASA?s Langley Research Center. From the results of these tests, a discussion is given of the baseline aircraft, its conventional control surfaces, and the distributed array. Each effector in the distributed array was tested individually as well as pre-determined configurations incorporating all 12 effectors on each wing. From the tests on the individual effectors, a method was created that allows for the prediction of the control authorities for any configuration of the array. The six pre-determined shapes served as bases for comparison to determine the accuracy of the prediction scheme. Additionally, the shapes were compared to the conventional control surfaces to determine if a distributed array could completely replace those control surfaces.
Identifer | oai:union.ndltd.org:NCSU/oai:NCSU:etd-03272007-011124 |
Date | 26 April 2007 |
Creators | Lion, Stephen Todd |
Contributors | Charles Hall, Ashok Gopalarathnam, James Selgrade |
Publisher | NCSU |
Source Sets | North Carolina State University |
Language | English |
Detected Language | English |
Type | text |
Format | application/pdf, application/zip |
Source | http://www.lib.ncsu.edu/theses/available/etd-03272007-011124/ |
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