Journal of Aircraft

Papers
(The median citation count of Journal of Aircraft is 0. 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 2021-06-01 to 2025-06-01.)
ArticleCitations
Effect of Partial Ground and Partial Ceiling on Propeller Performance24
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration18
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data16
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail16
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips16
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales15
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft14
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition14
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing14
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion14
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data14
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport13
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection12
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft11
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions11
System Identification of a Subscale Distributed Electric Propulsion Aircraft10
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance10
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems9
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels9
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings8
Advances in Aircraft System Identification at NASA Langley Research Center8
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts8
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage8
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft8
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization8
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling8
Efficient Algorithm of Real-Time Failure Probability Function Updating7
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning7
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads7
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters7
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio7
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover7
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification7
Wind Tunnel Testing of Tethered Inflatable Wings7
Investigation on “Replacing Bolts with Rivets” in Composite Structures7
Flight-Test Determination of Longitudinal Stability Using System Identification7
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers6
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft6
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data5
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”5
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers5
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes5
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results5
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions5
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft5
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering5
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method5
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research5
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints5
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary5
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale5
Economic Aspects of Aircraft Propulsion Electrification5
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method4
Fluidic Flow Control Devices for Gust Load Alleviation4
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus4
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design4
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics4
Energy-Harvesting Performance of an Aircraft Propeller4
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water4
Machine Learning Models for Multirotor Performance Prediction4
Numerical Simulation of the Common Research Model with Natural Laminar Flow4
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV4
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps4
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow4
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion4
Transonic Flutter Dips of the AGARD 445.6 Wing4
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes4
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface4
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X4
Experimental and Computational Investigation of Rotor Noise in Hover4
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging4
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft4
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel4
Ice Shape Convergence in Multistep Ice Accretion Simulations4
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor4
Announcements and Acknowledgments4
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation3
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids3
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method3
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft3
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions3
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics3
Autorotation-Based Descent with Trajectory Optimization3
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles3
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model3
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System3
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions3
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection3
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation3
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage3
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles3
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis3
Control-Oriented Modeling for Flexible Aircraft3
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows3
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks2
Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds2
Correction: Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design2
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model2
Improving Structural Test and Analysis Correlation Using Digital Image Correlation Boundary Measurements2
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies2
Insights and Lessons Learned from the NASA Juncture Flow Experiment2
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings2
Estimating Aircraft Landing Weights from Mode S Data2
Preliminary Design Criteria for Supersonic Biplane2
Liquid Cooling Systems for Batteries of Electric Vertical Takeoff and Landing Aircraft2
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics2
Understanding High-Speed Aeroelastic Stability of a Gimballed Proprotor2
Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion2
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing2
Aerodynamic Characteristics of Unmanned Aerial Vehicle with Z-Shaped Folding Wings2
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter2
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective2
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation2
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport2
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D2
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration2
Quantifying Impacts of Uncertainties on Certification-Driven Design2
Uncertainty Propagation of Optimal Hybrid-Electric Aircraft Designs in Scenario-Based Framework2
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction2
Efficient Aerostructural Wing Optimization Considering Mission Analysis2
Introduction to the Fourth AIAA High-Lift Prediction Workshop Virtual Collection2
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests2
Advancements in the Theory and Practice of Flight Vehicle System Identification2
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments2
Controlled Flow in a Serpentine Diffuser with a Cowl Inlet2
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core2
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing2
Benefits and Challenges of Electric Propulsion for Commuter Aircraft2
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data2
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data2
Effect of Squeezing Force on Stress and Fatigue of Aircraft Riveted Joints2
Polynomial Chaos Kriging Models for Uncertainty Quantification in High-Speed Flow Applications2
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion2
Aerodynamic Design of Prop-Rotor Blades Using Neural Networks2
Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling1
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data1
Dynamic Stability of the Hybrid Airship Influenced by Added Mass Effect1
Optimal Mission Profile for Low-Boom Supersonic Aircraft1
End-to-End Uncertainty Quantification with Analytical Derivatives for Design Under Uncertainty1
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics1
Deterministic and Probabilistic Approaches to Model and Update Dynamic Systems1
Retrofit Measures for Aircraft Noise Reduction: Simulation Benchmark and Impact Assessment1
Stability of Gossamer Propellers for High-Altitude Ballooning1
Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System1
Method for Quantifying Pollutant Emissions Within Preliminary Design of Small Aircraft1
Low-Order Modeling of Stacked Rotor Performance in Hover1
Exploration of a Low-Speed, Flapped, Slotted, Natural-Laminar-Flow Airfoil1
Design Exploration of a Distributed Electric Propulsion Aircraft Using Explainable Surrogate Models1
Unsteady Effects of Blowing over Actuated Surfaces Using Phase-Locked Particle Image Velocimetry1
Unsteady Propeller Wake Interference on Wing in Tractor Configuration at Low-Reynolds-Number Condition1
Application of Mass Particle Methods in the Shape Design for Scientific Balloons1
Off-Design Performance Analysis of a Parallel Hybrid Electric Regional Turboprop Aircraft1
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming1
Flutter Calculations Using the Unsteady Source and Doublet Panel Method1
Study on the Anti-Icing of Conical Rotating Spinners with Different Cone Angles1
Quality-Informed Test Design for Wind Tunnel Testing1
Assessment of Aerodynamic Torque on Propeller Whirl Flutter and Its Control1
Scale Resolving Simulation of Buffet Effects Induced by Ultrahigh Bypass Ratio Nacelle Installation1
High Crosswind-Tolerance Airplane by Adjusting Dihedral Angle and Vertical Tail Volume1
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control1
Propeller Ceiling Effect in Forward Flight1
Letter from the Editor1
Comparative Research on Landing and Rollout Characteristics of Skid-Equipped and Wheeled Aircraft1
Assessing the Feasibility of Hydrogen-Powered Aircraft: A Comparative Economic and Environmental Analysis1
Numerical Investigation of Ice Formation on a Wing with Leading-Edge Tubercles1
Numerical Simulation of the Flow in the ONERA F1 Wind Tunnel1
Aeropropulsive Shape Optimization of an Airfoil System in the Transonic Regime1
Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft1
Integrated Three-Dimensional Airloads and Stresses on Lift-Offset Coaxial Rotors at Extreme Speeds1
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap1
Effect of Angle of Attack on Propeller Aeroacoustics at Positive and Negative Thrust1
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft1
Overview of System Identification Tool Advancements at Systems Technology, Incorporated1
About the Wing and Whirl Flutter of a Slender Wing–Propeller System1
Results from the Second Ice Prediction Workshop by Using the CIRA Cartesian Method1
Statistical Approach for Electric Taxiing Requirements for Regional Turboprop Aircraft1
Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification1
Reynolds-Averaged Studies of the Sandia Transonic Bump Validation Challenge, with Loss of Symmetry1
Multifidelity Design of Structurally Embedded Waveguides1
Experimental Results for a Low-Reynolds-Number Airfoil in a Low-Turbulence Wind Tunnel1
Laminar–Turbulent Transition Prediction on Industrial Computational Fluid Dynamics Applications1
Transonic Shock Buffet Flowfield Assessment Using Various Dynamic Mode Decomposition Techniques1
Aircraft Parameter Estimation Considering Process and Measurement Noise1
Airfoil Separation Constraint Formulation for Aerodynamic Shape Optimization1
Estimation of the Fan Rotational Speed Using Flyover Audio Recordings1
Design of Hybrid-Laminar-Flow-Control Wing and Suction System for Transonic Midrange Aircraft1
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America1
Numerical Modeling of Aircraft Fire: Postcrash Fire1
Statistical Analysis of the Surface Roughness on Aircraft Icing1
Active Hinged Wingtip Control for Reducing Wing Root Bending Moment1
Nonlinear Multibody Modeling of Flexible Aircraft with Flared Hinged Wingtips1
Design and Aerodynamic Analysis of Leading Edge for Morphing Wing1
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact1
Robust Optimization of a Thermal Anti-Ice Protection System in Uncertain Cloud Conditions1
Fundamental Concepts of Boundary-Layer Ingestion Propulsion0
Planform Mesh Requirements for Fixed and Rotating Wing with Separation0
System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains0
Advances and Modern Applications of Frequency-Domain Aircraft and Rotorcraft System Identification0
Flowfield of an S-Shaped Inlet with High Boundary-Layer Ingestion Fraction0
Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design0
Aerodynamic Design of Shock Control Bumps on an Aircraft Considering Structural Constraints0
Three-Dimensional Aeromechanical Analysis of Lift Offset Coaxial Rotors: A Helios Test Case0
Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter0
Further Noise Reduction of Regional Jet Two-Wheel Main Landing Gear0
Configuration Estimation from Position Data of Civil Jet Aircraft for Noise Mapping0
High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring0
Sizing and Analysis of a Lift-Plus-Cruise Aircraft with Electrified Propulsion0
Implementation of Fuel-Saving Relaxed Climb Procedure0
Summary of the 4th High-Lift Prediction Workshop Hybrid RANS/LES Technology Focus Group0
Modeling of Hovering Intermeshing Rotor Using Blade Element Momentum Theory0
Fourth High-Lift Prediction/Third Geometry and Mesh Generation Workshops: Overview and Summary0
Impact of Airframe–Propulsion System Modeling Strategies on Key Structural Performance Metrics0
Nonlinear Unsteady Aerodynamic Reduced-Order Modeling Using a Surrogate-Based Recurrent Framework0
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft0
Powered Low-Speed Experimental Aerodynamic Investigation of an Over-Wing-Mounted Nacelle Configuration0
Variable Noise Reduction Systems for a Notional Supersonic Business Jet0
Steady and Unsteady Hover Test of a Lift Compounding Rotorcraft0
Numerical Simulation of the High-Speed Leg of the National Transonic Facility0
Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics0
Steady Versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration0
Macro- and Mesoscopic Design for Cabin Door Pretightened Fabric Rubber Seal Structure0
Sprayed Liquid Flaps: A Numerical Assessment of a Multiphase Jet Concept0
Design Exploration of Transonic Airfoils for Natural and Hybrid Laminar Flow Control Applications0
Antidisturbance Slip Ratio Algorithm of Aircraft Braking System Based on On/Off Valves0
Numerical Analysis of Low-Reynolds-Number Flows in Earth and Mars Atmosphere0
Fluid–Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft0
Aircraft Load Estimation Using Linear Parameter-Varying System-Based Hybrid Observers0
Effects of Wave Parameters on Load Reduction Performance for Amphibious Aircraft with V-Hydrofoil0
Multifidelity Aeroelastic Model for Corrugated Morphing Structures0
Experimental and Numerical Nonlinear Stability Analysis of Wings Incorporating Flared Folding Wingtips0
Individual Blade Control Approach for Active Vibration Suppression of a Lift-Offset Coaxial Rotorcraft0
Numerical Analysis of Porpoising Stability Limit of a Blended-Wing–Body Aircraft During Ditching0
Examination of End Plate Sizing for Reflection Plane Wind-Tunnel Testing0
Steady Solutions for Supersonic Transport Takeoffs with a Variable Noise Reduction System0
Geometric Design of Hypersonic Vehicles for Optimal Mission Performance with High-Fidelity Aerodynamic Models0
Investigation of Aerodynamic Support Interference for Testing a Semispan T Tail Aircraft Model0
Finite Element Model Tuning Using Analytical Sensitivity Values0
High-Fidelity Simulations of a Slotted, Natural-Laminar-Flow Wing Section0
Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions0
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing0
Correlation of High-Speed Tiltrotor Stability Predictions with Test Data and Parametric Study0
2025 AIAA Journal of Aircraft Editorial0
Experimental and Numerical Investigations of Mini-Tab Device for Active Flow Control0
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft0
Impact of Phase Offset on the Flowfields Downstream of Synchronized Propellers0
Fourth AIAA High-Lift Prediction Workshop: Fixed-Grid Reynolds-Averaged Navier–Stokes Summary0
Enhanced Aircraft Wake Decay Under Crosswind Conditions0
Design of the Truss Wing Structure Based on Principal Stress Trajectory Method0
Two-Dimensional Static Margin for Three-Dimensional Aircraft0
Flow Control Devices for Aeroacoustic Noise Suppression in Cavity Flow0
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