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http://dx.doi.org/10.3795/KSME-B.2006.30.10.1012

Static Wind Tunnel Test of Smart Un-manned Aerial Vehicle(SUAV) for TR-S4 Configuration  

Choi Sung-Wook (한국항공우주연구원 스마트무인기사업단)
Kim Cheol-Wan (한국항공우주연구원 공력성능그룹)
Lee Jang-Yeon (한국항공우주연구원 공력성능그룹)
Chung Jin-Deog (한국항공우주연구원 공력성능그룹)
Publication Information
Transactions of the Korean Society of Mechanical Engineers B / v.30, no.10, 2006 , pp. 1012-1018 More about this Journal
Abstract
To evaluate the aerodynamic efficiency of TR-S4 configuration, wind tunnel tests of 40% scaled model were done in KARI LSWT. TR-S4 configuration has different nacelle shape, larger EO/IR camera and aftward wing location compared with TR-S2. Component build-up test after adding each element of model is performed. Also effects of horizontal tail incidences, Flaperon and Aileron deflection. on aerodynamic characteristics are measured. Test results showed that TR-S4 configuration has favorable stability characteristics in longitudinal, lateral and directional for the pitch and yaw motions.
Keywords
Wind Tunnel Testing; SUAV; High Lift Device; Flaperon; Stability; Tail Incidence;
Citations & Related Records
Times Cited By KSCI : 6  (Citation Analysis)
연도 인용수 순위
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