受强制性开放获取政策约束的文章 - Eli Livne了解详情
无法在其他位置公开访问的文章：2 篇
Design-Oriented Computational Fluid Dynamics-Based Unsteady Aerodynamics for Flight-Vehicle Aeroelastic Shape Optimization
PC Chen, Z Zhang, E Livne
AIAA Journal 53 (12), 3603-3619, 2015
强制性开放获取政策： US National Aeronautics and Space Administration
Probabilistic aeroservoelastic reliability assessment considering control system component uncertainty
S Wu, E Livne
Aiaa Journal 54 (8), 2507-2520, 2016
强制性开放获取政策： US National Aeronautics and Space Administration
可在其他位置公开访问的文章：10 篇
Wind tunnel investigation of a flexible wing high-lift configuration with a variable camber continuous trailing edge flap design
NT Nguyen, N Precup, E Livne, JM Urnes, E Dickey, C Nelson, J Chiew, ...
33rd AIAA Applied Aerodynamics Conference, 2417, 2015
强制性开放获取政策： US National Aeronautics and Space Administration
Supersonic Configurations at Low Speeds (SCALOS): Test/Simulation Correlation Studies
N Mavriplis, KY Ting, A Moustafa, C Hill, R Soltani, CP Nelson, E Livne
AIAA Scitech 2022 Forum, 1801, 2022
强制性开放获取政策： US National Aeronautics and Space Administration
Supersonic Configurations at Low Speeds (SCALOS): Project Background and Progress at University of Washington
CP Nelson, KY Ting, N Mavriplis, R Soltani, E Livne
AIAA Scitech 2022 Forum, 1803, 2022
强制性开放获取政策： US National Aeronautics and Space Administration
The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration
N Precup, M Mor, E Livne
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015
强制性开放获取政策： US National Aeronautics and Space Administration
Supersonic Configurations at Low Speeds (SCALOS): Model Geometry and Aerodynamic Results
KY Ting, N Mavriplis, R Soltani, CP Nelson, E Livne
AIAA Scitech 2022 Forum, 1800, 2022
强制性开放获取政策： US National Aeronautics and Space Administration
Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System
NT Nguyen, NB Cramer, KE Hashemi, MC Drew, J Xiong, T Mundt, M Mor, ...
AIAA Scitech 2020 Forum, 0214, 2020
强制性开放获取政策： US National Aeronautics and Space Administration
Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System
NT Nguyen, NB Cramer, KE Hashemi, E Ting, M Drew, R Wise, ...
AIAA Aviation 2019 Forum, 3156, 2019
强制性开放获取政策： US National Aeronautics and Space Administration
Aerostructural design optimization of a flexible wing aircraft with continuous morphing trailing edge
GE Fujiwara, NT Nguyen, E Livne, MB Bragg
2018 Multidisciplinary Analysis and Optimization Conference, 3571, 2018
强制性开放获取政策： US National Aeronautics and Space Administration
Uncertainty analysis of flutter predictions with focus on the AGARD 445.6 wing
S Wu, E Livne
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
强制性开放获取政策： US National Aeronautics and Space Administration
Aeroservoelastic Simulation Considering Control System Component Uncertainty
S Wu, E Livne
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015
强制性开放获取政策： US National Aeronautics and Space Administration
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