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Research on landing gear strut damping orifice design based..:

, In: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022),

Li, S. ; Li, L. ; Wang, H.. - p. None , 2022

Link: https://doi.org/10.1049/icp.2022.1774

RT 
T1 <cTitle>CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022)</cTitle>: T1 <Title>Research on landing gear strut damping orifice design based on nurbs for optimizing aircraft ground dynamics</Title>

UL https://suche.suub.uni-bremen.de/peid=ieee-9946150&Exemplar=1&LAN=DE
				
A1 Li, S.
A1 Li, L.
A1 Wang, H.
A1 Xie, D.
YR 2022
K1 aircraft
K1 damping
K1 design engineering
K1 hydraulic systems
K1 optimisation
K1 orifices (mechanical)
K1 splines (mathematics)
K1 aircraft ground dynamics
K1 NURBS parameterization
K1 strut hydraulic orifice
K1 lower peak dynamic load condition
K1 aircraft structure mass weight
K1 landing gear strut damping orifice design
K1 shock strut
K1 shock energy
K1 nonuniform rational B-splines
K1 algorithm optimization
K1 generative method
K1 aircraft landing gear hydraulic damping orifice design
K1 aircraft landing gear strut hydraulic
K1 multiobjective optimization
SP None
LK http://dx.doi.org/https://doi.org/10.1049/icp.2022.1774
DO https://doi.org/10.1049/icp.2022.1774
SF ELIB - SuUB Bremen

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