Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing

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Publisher
AMER INST AERONAUTICS ASTRONAUTICS
Issue Date
2015-03
Language
English
Article Type
Article
Citation

JOURNAL OF AIRCRAFT, v.52, no.2, pp.713 - 718

ISSN
0021-8669
DOI
10.2514/1.C032747
URI
http://hdl.handle.net/10203/201012
Appears in Collection
AE-Journal Papers(저널논문)
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