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1 Ergebnisse
1
Development of wind tunnel dynamic test system for coupled ..:
, In:
CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022)
,
Tan, H.
;
Wang, J.
;
Bu, C.
... - p. None , 2022
Link:
https://doi.org/10.1049/icp.2022.1578
RT T1
CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022)
: T1
Development of wind tunnel dynamic test system for coupled motion with multi-degrees of freedom
UL https://suche.suub.uni-bremen.de/peid=ieee-9946182&Exemplar=1&LAN=DE A1 Tan, H. A1 Wang, J. A1 Bu, C. A1 Mu, W. A1 Shen, Y. A1 Chen, H. YR 2022 K1 aerodynamics K1 aerospace components K1 aircraft K1 aircraft control K1 design engineering K1 position control K1 servomechanisms K1 vehicle dynamics K1 wind tunnels K1 wind tunnel dynamic test system K1 multidegrees K1 complex aerodynamic data K1 advanced layout aircraft K1 AVIC Aerodynamics Research Institute K1 three-degree-of-freedom K1 amplitude oscillation test system K1 FL-51 low speed wind tunnel K1 oscillation device K1 drive control system K1 hydraulic power system K1 design input K1 hardware scheme design K1 drive system K1 position servo control algorithm K1 performance index debugging K1 wing layout aircraft model K1 excellent dynamic performance K1 test data K1 multidegree-of-freedom coupled motion test K1 aircraft development K1 size 1.5 m K1 velocity 60.0 m/s SP None LK http://dx.doi.org/https://doi.org/10.1049/icp.2022.1578 DO https://doi.org/10.1049/icp.2022.1578 SF ELIB - SuUB Bremen
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