Journal of Aircraft

Papers
(The TQCC of Journal of Aircraft is 2. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2020-10-01 to 2024-10-01.)
ArticleCitations
Research Initiative for Numerical and Experimental Studies on High-Speed Stall of Civil Aircraft11
Impact of Low-Order Modeling on Aeroelastic Predictions for Very Flexible Wings11
Sizing of High-Aspect-Ratio Wings with Folding Wingtips10
Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion9
Fourth High-Lift Prediction/Third Geometry and Mesh Generation Workshops: Overview and Summary9
On the Effect of Geometric Nonlinearity on the Dynamics of Flared Folding Wingtips8
HLPW-4: Wall-Modeled Large-Eddy Simulation and Lattice–Boltzmann Technology Focus Group Workshop Summary8
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft7
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft7
System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains7
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data6
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing6
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration6
Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft6
Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft6
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft6
Design Exploration of Transonic Airfoils for Natural and Hybrid Laminar Flow Control Applications6
Approach for Aerodynamic Gust Load Alleviation by Means of Spanwise-Segmented Flaps5
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads5
Effect of Partial Ground and Partial Ceiling on Propeller Performance5
Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System5
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America5
Variable Noise Reduction Systems for a Notional Supersonic Business Jet5
Sizing and Analysis of a Lift-Plus-Cruise Aircraft with Electrified Propulsion5
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance5
Wind Tunnel and Grid Resolution Effects in Large-Eddy Simulations of the High-Lift Common Research Model4
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data4
Data-Driven Modeling for Transonic Aeroelastic Analysis4
System Identification of a Subscale Distributed Electric Propulsion Aircraft4
Aerodynamic Optimization and Fuel Burn Evaluation of a Transonic Strut-Braced-Wing Single-Aisle Aircraft4
HLPW-4/GMGW-3: Mesh Adaptation for RANS Technology Focus Group Workshop Summary4
Development of an Aeromechanics Solver for Loads and Stability of Hingeless Tiltrotors4
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion4
Modern Implementation and Evaluation of Lifting-Line Theory for Complex Geometries4
Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration4
Unmanned Wingless Rotorcraft Scaling4
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions3
On Improved Understanding of Airfoil Performance Evaluation Methods at Low Reynolds Numbers3
Multifidelity Aeroelastic Model for Corrugated Morphing Structures3
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data3
Fleet Design Optimization of Package Delivery Unmanned Aerial Vehicles Considering Operations3
Advancements in the Theory and Practice of Flight Vehicle System Identification3
Insights and Lessons Learned from the NASA Juncture Flow Experiment3
Macro- and Mesoscopic Design for Cabin Door Pretightened Fabric Rubber Seal Structure3
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact3
Airfoil Morphed Leading-Edge Design for High-Lift Applications Using Genetic Algorithm3
Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter3
Methodology for Preliminary Flight Control Actuator Design3
Real-Time Simulation of a Shipborne Rotor via Linearized State-Space Free-Vortex Wake Models2
Laminar–Turbulent Transition Prediction on Industrial Computational Fluid Dynamics Applications2
Summary of the 4th High-Lift Prediction Workshop Hybrid RANS/LES Technology Focus Group2
Antidisturbance Slip Ratio Algorithm of Aircraft Braking System Based on On/Off Valves2
Analytical and Experimental Power Minimization for Fixed-Pitch Coaxial Rotors in Hover2
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics2
Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations2
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection2
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction2
Exploring Design Options for Wing Leading Edge Against Bird Strike2
Numerical Simulation of the Common Research Model with Natural Laminar Flow2
Experimental and Computational Investigation of Rotor Noise in Hover2
Determining Region of Installation of Flat-Ended Piezoelectric De-Icing Actuators on Curved Surfaces2
Finite Element Model Updating for Very Flexible Wings2
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels2
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization2
Scoring Approach to Assess Maintenance Risk for Aircraft Systems in Conceptual Design2
Plasma Gurney Flap Flight Control at Low Angle of Attack2
Geometric Design of Hypersonic Vehicles for Optimal Mission Performance with High-Fidelity Aerodynamic Models2
Letter from the Editor2
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary2
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results2
Aircraft Flutter and Aerodynamic Work2
Estimating Aircraft Landing Weights from Mode S Data2
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap2
Remote Uncorrelated Pilot Input Excitation Assessment for Unmanned Aircraft Aerodynamic Modeling2
Numerical Analysis of Porpoising Stability Limit of a Blended-Wing–Body Aircraft During Ditching2
Efficient Aerostructural Wing Optimization Considering Mission Analysis2
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet2
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