Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System
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Eli Livne | Marat Mor | Nhan T. Nguyen | Michael C. Drew | Nick B. Cramer | Juntao Xiong | Kelley E. Hashemi | Tyler Mundt | Nick Cramer | E. Livne | N. Nguyen | J. Xiong | M. Mor | M. Drew | T. Mundt
[1] T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .
[2] Nhan T. Nguyen,et al. Development of an Aeroservoelastic Model for Gust Load Alleviation of the NASA Common Research Model Wind Tunnel Experiment , 2020 .
[3] Nhan T. Nguyen,et al. A Multi-Objective Flight Control Approach for Performance Adaptive Aeroelastic Wing , 2015 .
[4] Nhan T. Nguyen,et al. Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft , 2020 .
[5] Moffett Field,et al. Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency , 2013 .
[6] Sonia Lebofsky,et al. Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design , 2014 .
[7] John C. Vassberg,et al. Development of a Common Research Model for Applied CFD Validation Studies , 2008 .
[8] Sonia Lebofsky,et al. Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design , 2015 .
[9] Nhan Nguyen,et al. Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency , 2013 .
[10] James M. Urnes,et al. Active Control for Elastic Wing Structure Dynamic Modes , 2015 .
[11] Eric Ting,et al. A Mission-Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift-to-Drag Ratios of Future N+3 Transport Aircraft , 2013 .
[12] Nhan T. Nguyen,et al. Simulation and Modeling of Flow Generated by Gust Generator in a Wind Tunnel , 2020 .
[13] Eli Livne,et al. Design, construction, and tests of an aeroelastic wind tunnel model of a variable camber continuous trailing edge flap (VCCTEF) concept wing , 2014 .
[14] Eric Ting,et al. Real-Time Adaptive Least-Squares Drag Minimization for Performance Adaptive Aeroelastic Wing , 2016 .
[15] Nhan T. Nguyen,et al. Multi-Objective Adaptive Control for Load Alleviation and Drag Minimization of Flexible Aircraft , 2018 .
[16] Eli Livne,et al. An Active Variable Camber Continuous Trailing Edge Flapped Wing Wind Tunnel Model for Aeroelastic "In-Flight" Shape Optimization Tests , 2018, 2018 Multidisciplinary Analysis and Optimization Conference.
[17] Nhan Nguyen,et al. Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction , 2012 .
[18] J. Anderson,et al. Fundamentals of Aerodynamics , 1984 .
[19] Robert T Jones,et al. Operational treatment of the nonuniform-lift theory in airplane dynamics , 1938 .
[20] Eli Livne,et al. 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 , 2015 .
[21] Nhan Nguyen,et al. NASA Innovation Fund 2010 Project Elastically Shaped Future Air Vehicle Concept , 2010 .
[22] Eric Ting,et al. Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System , 2019, AIAA Aviation 2019 Forum.
[23] Eric Ting,et al. Active Gust Load Alleviation of High-Aspect Ratio Flexible Wing Aircraft , 2018 .
[24] Eric Ting,et al. Optimization of Variable-Camber Continuous Trailing-Edge Flap Configuration for Drag Reduction , 2018, Journal of Aircraft.
[25] Nhan T. Nguyen,et al. Multi-objective Optimal Control of the 6-DoF Aeroservoelastic Common Research Model with Aspect Ratio 13.5 Wing , 2019 .