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Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
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Outgoing claims: the papers this work cites, builds on, or argues with.
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LIMIT-CYCLE OSCILLATIONS IN HIGH-ASPECT-RATIO WINGS
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On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings
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Numerical Investigation of Nonlinear Aeroelastic Effects on Flexible High-Aspect-Ratio Wings
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Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow
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Experiments and analysis for composite blades under large deflections. II - Dynamic behavior
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Flight dynamics of aeroelastic vehicles
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Aeroelastic characteristics of a highly flexible aircraft
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Finite state induced flow models. I - Two-dimensional thin airfoil
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Nonlinear Aeroelasticity and Chaos
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Aeroelastic tailoring of composite box beams
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Nonlinear aeroelastic response of an airfoil
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Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings
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Finite Element Solution of Nonlinear Intrinsic Equations for Curved Composite Beams
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Finite-State Airloads for Deformable Airfoils on Fixed and Rotating Wings
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Wing Flutter Simulations Using an Aeroelastic Solver Based on the Predictor—Corrector Scheme
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Time-domain Analytical Method for Aeroelastic Analysis of High Aspect Ratio Wing Using Unsteady Indicial Aerodynamics
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3D Dynamic Modal Rotations Method for Large Structural Deformations of Slender Bodies
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Nonlinear Aeroelastic Modeling of a Flexible Wing and Comparison with Experiments
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Effects of Geometric Nonlinearities on the Fidelity of Aeroelasticity Loads Analyses of Very Flexible Airframes
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Trajectory control of a very flexible flying wing
inferred← citeshttps://doi.org/10.23919/acc.2018.8430956openalex-snapshot
Model Predictive Control for Aircraft Load Alleviation: Opportunities and Challenges
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Automatic Landing Control of a Very Flexible Flying Wing
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Effects of Span Morphing on Flutter Characteristics of Subsonic Wing
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Limit cycle oscillation prediction based on Finite Element-Modal approach
inferred← citeshttps://doi.org/10.2514/1.15566openalex-snapshot
Aeroelasticity of Nonlinear Structures Using the Corotational Method
inferred← citeshttps://doi.org/10.2514/1.2273openalex-snapshot
Aeroelasticity of Nonconventional Airplane Configurations -Past and Future
inferred← citeshttps://doi.org/10.2514/1.25814openalex-snapshot
Stability and Control of a High-Altitude, Long-Endurance UAV
inferred← citeshttps://doi.org/10.2514/1.27606openalex-snapshot
Nonlinear Flight Dynamics of Very Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.30890openalex-snapshot
Flight Dynamics of Highly Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.34797openalex-snapshot
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces
inferred← citeshttps://doi.org/10.2514/1.36150openalex-snapshot
Modified Inertially Coupled Equations of Motion for a Flexible Aircraft with Coupled Vibrations
inferred← citeshttps://doi.org/10.2514/1.45334openalex-snapshot
Multibody Dynamic Approach of Flight Dynamics and Nonlinear Aeroelasticity of Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.45406openalex-snapshot
Efficient Numerical Aeroelastic Analysis of a High-Aspect-Ratio Wing Considering Geometric Nonlinearity
inferred← citeshttps://doi.org/10.2514/1.46974openalex-snapshot
Validation Studies for Aeroelastic Trim and Stability of Highly Flexible Aircraft
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Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
inferred← citeshttps://doi.org/10.2514/1.6544openalex-snapshot
Numerical Investigation of Nonlinear Aeroelastic Effects on Flexible High-Aspect-Ratio Wings
inferred← citeshttps://doi.org/10.2514/1.c000265openalex-snapshot
Load Alleviation on a Joined-Wing Unmanned Aircraft
inferred← citeshttps://doi.org/10.2514/1.c031955openalex-snapshot
Engine Placement Effect on Nonlinear Trim and Stability of Flying Wing Aircraft
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Reexamined Structural Design Procedures for Very Flexible Aircraft
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Strain-Based Analysis for Geometrically Nonlinear Beams: A Modal Approach
inferred← citeshttps://doi.org/10.2514/1.c033435openalex-snapshot
Effect of Inertial and Constitutive Properties on Body-Freedom Flutter for Flying Wings
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Optimum Wing Shape of Highly Flexible Morphing Aircraft for Improved Flight Performance
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Modeling of Highly Flexible Multifunctional Wings for Energy Harvesting
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Nonlinear Static Aeroelasticity of High-Aspect-Ratio-Wing Aircraft by Finite Element and Multibody Methods
inferred← citeshttps://doi.org/10.2514/1.c033846openalex-snapshot
Concurrent Active Piezoelectric Control and Energy Harvesting of Highly Flexible Multifunctional Wings
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Finite-Element-Based Modeling for Flight Dynamics and Aeroelasticity of Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.c034162openalex-snapshot
Stability of Very Flexible Aircraft with Coupled Nonlinear Aeroelasticity and Flight Dynamics
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Aeroelastic Stability Analysis of Damaged High-Aspect-Ratio Composite Wings
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Industrially Inspired Gust Loads Analysis of Various-Aspect-Ratio Wings Featuring Geometric Nonlinearity
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Distributed Pressure Sensing–Based Flight Control for Small Fixed-Wing Unmanned Aerial Systems
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Testing of Folding Wingtip for Gust Load Alleviation of Flexible High-Aspect-Ratio Wing
inferred← citeshttps://doi.org/10.2514/1.c035901openalex-snapshot
Simulation and Optimization of Takeoff Maneuvers of Very Flexible Aircraft
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Impact of Low-Order Modeling on Aeroelastic Predictions for Very Flexible Wings
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Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration
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Experimental Evaluation of the ASWING Aeroelastic Framework: Aerodynamics and Propeller Models
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Experimental Evaluation of the ASWING Aeroelastic Framework: Structure Model
inferred← citeshttps://doi.org/10.2514/1.g000715openalex-snapshot
Dynamic Load Alleviation in Wake Vortex Encounters
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Gain-Scheduling Control of Flexible Aircraft with Actuator Saturation and Stuck Faults
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Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools
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Flight Control for Very Flexible Aircraft Using Model-Free Adaptive Control
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Code-to-Code Benchmark for Simulation Tools Based on the Unsteady Vortex-Lattice Method
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Gust Response for Flexibly Suspended High-Aspect Ratio Wings
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Dynamic Response of Highly Flexible Flying Wings
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X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
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Assessment of Wake-Tail Interference Effects on the Dynamics of Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.j051697openalex-snapshot
Robust Gust Alleviation and Stabilization of Very Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.j052316openalex-snapshot
Consistent Structural Linearization in Flexible Aircraft Dynamics with Large Rigid-Body Motion
inferred← citeshttps://doi.org/10.2514/1.j052684openalex-snapshot
Reduced-Order Aeroelastic Models for Dynamics of Maneuvering Flexible Aircraft
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Nonlinear Modal Aeroservoelastic Analysis Framework for Flexible Aircraft
inferred← citeshttps://doi.org/10.2514/1.j055721openalex-snapshot
Optimal Rolling Maneuvers with Very Flexible Wings
inferred← citeshttps://doi.org/10.2514/1.j056068openalex-snapshot
Continuous-Time State-Space Unsteady Aerodynamic Modeling for Efficient Loads Analysis
inferred← citeshttps://doi.org/10.2514/1.j056141openalex-snapshot
Aeroservoelastic Optimisation of Aerofoils with Compliant Flaps via Reparameterization and Variable Selection
inferred← citeshttps://doi.org/10.2514/1.j056804openalex-snapshot
Nonlinear Static Aeroelastic and Trim Analysis of Highly Flexible Joined-Wing Aircraft
inferred← citeshttps://doi.org/10.2514/1.j057309openalex-snapshot
Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems
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