Journal of Aircraft

Papers
(The median citation count of Journal of Aircraft is 1. 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 2020-11-01 to 2024-11-01.)
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
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration7
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft7
System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains7
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft7
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing6
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
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data6
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
Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter3
Methodology for Preliminary Flight Control Actuator Design3
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
Efficient Aerostructural Wing Optimization Considering Mission Analysis2
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet2
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
Remote Uncorrelated Pilot Input Excitation Assessment for Unmanned Aircraft Aerodynamic Modeling2
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
Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations2
Numerical Analysis of Porpoising Stability Limit of a Blended-Wing–Body Aircraft During Ditching2
Optimal Performance Trim Procedure for Multirotor Vertical Takeoff and Landing Vehicles1
Aerostructural Optimization and Comparative Study of Twin-Fuselage and Strut-Braced-Wing Aircraft Configurations1
Advances and Modern Applications of Frequency-Domain Aircraft and Rotorcraft System Identification1
Study of Nonlinear Stiffness and Damping Effects on Shimmy and Flutter1
Ship Air-Wake Identification from Experimental Data for Automatic Deck Landing and Takeoff1
Low-Order Modeling of Stacked Rotor Performance in Hover1
Vacuum and Hover Tests of a Dihedral–Anhedral Tip Composite Rotor1
Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics1
Numerical Investigation of Ice Formation on a Wing with Leading-Edge Tubercles1
Advances in Aircraft System Identification at NASA Langley Research Center1
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers1
Blended Wing Body Configuration for Hydrogen-Powered Aviation1
Large-Eddy Simulation of Low-Reynolds-Number Flow Around Partially Porous Airfoils1
Turbulence Model Effects on Vortex Interaction Prediction on a Multiswept Delta Wing1
Liquid Cooling Systems for Batteries of Electric Vertical Takeoff and Landing Aircraft1
System Identification of Unmanned Air Systems at Texas A&M University1
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data1
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles1
Dynamic Response of Circulation Control for Step and Sinusoidal Inputs1
Fountain Flow Visualization in Quadrotor Wake Decreasing Rotor Thrust In-Ground Effect1
Piezoelectric-Actuator De-Icing Array Design Based on Structural Vibration Modes1
Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics1
Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle1
Comparison of Overwing and Underwing Nacelle Aeropropulsion Optimization for Subsonic Transport Aircraft1
Optimization and Decision-Making Framework for Small Unmanned Aircraft Systems Fleet Design1
Optimum Flap Deflection for Improved Aircraft Performance Using Surrogate Modeling1
Fast Nonlinear Static Aeroelasticity Method for High-Aspect-Ratio Wings at Different Mach Regimes1
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus1
Individual Blade Control Approach for Active Vibration Suppression of a Lift-Offset Coaxial Rotorcraft1
Transonic Shock Buffet Flowfield Assessment Using Various Dynamic Mode Decomposition Techniques1
Stitched Graphene Nanoplatelet Composites for Unitized Aerospace Structures1
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport1
Comparison of Linear Flexible Aircraft Model Structures on Large Flexible Tiltrotor Aircraft1
Three-Dimensional Aeromechanical Analysis of Lift Offset Coaxial Rotors: A Helios Test Case1
Modeling of Hovering Intermeshing Rotor Using Blade Element Momentum Theory1
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control1
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics1
Aeroelastic Analysis of Actuated Adaptive Wingtips Based on Pressure Actuation1
Investigation of Aerodynamic Support Interference for Testing a Semispan T Tail Aircraft Model1
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks1
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover1
Improvement of Helicopter Operations on Frigates Using the Coanda Effect1
Assessment of Potential Commercial Success of Business Jets with Natural Laminar Flow1
Numerical Simulation of the Flow in the ONERA F1 Wind Tunnel1
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration1
Integrated Three-Dimensional Airloads and Stresses on Lift-Offset Coaxial Rotors at Extreme Speeds1
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel1
Including Blade Elasticity into Frequency-Domain Propeller Whirl Flutter Analysis1
Semi-Continuous Descent Operation: A Fuel-Efficient Interval Management Algorithm1
Fluidic Flow Control Devices for Gust Load Alleviation1
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System1
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings1
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV1
Estimation of the Fan Rotational Speed Using Flyover Audio Recordings1
Numerical Evaluation on Large Ground-Effect Seaplane at Takeoff with Power Augmented Ram1
Deterministic and Probabilistic Approaches to Model and Update Dynamic Systems1
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems1
About the Wing and Whirl Flutter of a Slender Wing–Propeller System1
Automatic Continuous Thrust Control for Supersonic Transport Takeoff Noise Reduction1
Fourth AIAA High-Lift Prediction Workshop: Fixed-Grid Reynolds-Averaged Navier–Stokes Summary1
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles1
Multidisciplinary Design Optimization of Transonic Wings with Boundary-Layer Suction1
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions1
Methodology for Evaluating a Distributed Variable-Camber Trailing-Edge System in Preliminary Aircraft Design1
Robust Optimization of a Thermal Anti-Ice Protection System in Uncertain Cloud Conditions1
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics1
Enhanced Aircraft Wake Decay Under Crosswind Conditions1
A Study of the Wind Sensing Performance of Small Pusher and Puller Hexacopters1
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming1
Statistical Analysis of the Surface Roughness on Aircraft Icing1
Overview of System Identification Tool Advancements at Systems Technology, Incorporated1
DPW-7: Steady and Unsteady Computations of the Common Research Model at Different Reynolds Numbers1
Design and Characterization of High-Lift Capabilities for Slotted, Natural-Laminar-Flow Airfoils1
Control-Oriented Modeling for Flexible Aircraft1
Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification1
Retrospective and Recent Examples of Aircraft and Rotorcraft System Identification at DLR1
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