Journal of Aircraft

(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 2020-07-01 to 2024-07-01.)
Sizing of High-Aspect-Ratio Wings with Folding Wingtips10
Research Initiative for Numerical and Experimental Studies on High-Speed Stall of Civil Aircraft10
Impact of Low-Order Modeling on Aeroelastic Predictions for Very Flexible Wings10
Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion8
On the Effect of Geometric Nonlinearity on the Dynamics of Flared Folding Wingtips8
System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains7
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft7
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data7
Fourth High-Lift Prediction/Third Geometry and Mesh Generation Workshops: Overview and Summary6
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing6
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft6
Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft6
Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft6
HLPW-4: Wall-Modeled Large-Eddy Simulation and Lattice–Boltzmann Technology Focus Group Workshop Summary6
Sizing and Analysis of a Lift-Plus-Cruise Aircraft with Electrified Propulsion5
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads5
Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System5
Effect of Partial Ground and Partial Ceiling on Propeller Performance5
Variable Noise Reduction Systems for a Notional Supersonic Business Jet5
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration5
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft5
Design Exploration of Transonic Airfoils for Natural and Hybrid Laminar Flow Control Applications4
HLPW-4/GMGW-3: Mesh Adaptation for RANS Technology Focus Group Workshop Summary4
Unmanned Wingless Rotorcraft Scaling4
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion4
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data4
System Identification of a Subscale Distributed Electric Propulsion Aircraft4
Modern Implementation and Evaluation of Lifting-Line Theory for Complex Geometries4
Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration4
Advancements in the Theory and Practice of Flight Vehicle System Identification3
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America3
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance3
Aerodynamic Optimization and Fuel Burn Evaluation of a Transonic Strut-Braced-Wing Single-Aisle Aircraft3
Methodology for Preliminary Flight Control Actuator Design3
Macro- and Mesoscopic Design for Cabin Door Pretightened Fabric Rubber Seal Structure3
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact3
Approach for Aerodynamic Gust Load Alleviation by Means of Spanwise-Segmented Flaps3
Development of an Aeromechanics Solver for Loads and Stability of Hingeless Tiltrotors3
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions3
Aircraft Flutter and Aerodynamic Work2
Estimating Aircraft Landing Weights from Mode S Data2
Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations2
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap2
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data2
Fleet Design Optimization of Package Delivery Unmanned Aerial Vehicles Considering Operations2
Geometric Design of Hypersonic Vehicles for Optimal Mission Performance with High-Fidelity Aerodynamic Models2
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction2
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results2
Determining Region of Installation of Flat-Ended Piezoelectric De-Icing Actuators on Curved Surfaces2
Multifidelity Aeroelastic Model for Corrugated Morphing Structures2
Analytical and Experimental Power Minimization for Fixed-Pitch Coaxial Rotors in Hover2
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics2
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection2
Remote Uncorrelated Pilot Input Excitation Assessment for Unmanned Aircraft Aerodynamic Modeling2
Airfoil Morphed Leading-Edge Design for High-Lift Applications Using Genetic Algorithm2
Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter2
Antidisturbance Slip Ratio Algorithm of Aircraft Braking System Based on On/Off Valves2
Summary of the 4th High-Lift Prediction Workshop Hybrid RANS/LES Technology Focus Group2
Finite Element Model Updating for Very Flexible Wings2
Data-Driven Modeling for Transonic Aeroelastic Analysis2
Numerical Analysis of Porpoising Stability Limit of a Blended-Wing–Body Aircraft During Ditching2
Scoring Approach to Assess Maintenance Risk for Aircraft Systems in Conceptual Design2
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization2
Exploring Design Options for Wing Leading Edge Against Bird Strike2
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet2
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary2
Insights and Lessons Learned from the NASA Juncture Flow Experiment2