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 2021-08-01 to 2025-08-01.)
ArticleCitations
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration25
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips19
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales17
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data16
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data16
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition16
Effect of Partial Ground and Partial Ceiling on Propeller Performance16
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion16
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing15
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail14
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft14
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft13
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection13
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance12
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels12
System Identification of a Subscale Distributed Electric Propulsion Aircraft12
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft11
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings11
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts10
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport10
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling9
Advances in Aircraft System Identification at NASA Langley Research Center9
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft9
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization9
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions9
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems9
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing8
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters8
Efficient Algorithm of Real-Time Failure Probability Function Updating8
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads7
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification7
Interaction Between a Hovering Maritime Helicopter and Ship Exhaust Plume7
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage7
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio7
Wind Tunnel Testing of Tethered Inflatable Wings7
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results7
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers7
Investigation on “Replacing Bolts with Rivets” in Composite Structures7
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning7
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft7
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research7
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft6
Economic Aspects of Aircraft Propulsion Electrification6
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”6
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints6
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data6
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover6
Flight-Test Determination of Longitudinal Stability Using System Identification6
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions6
Gust Response Predictions of a Very Flexible Wing Model6
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design5
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV5
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method5
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method5
Numerical Simulation of the Common Research Model with Natural Laminar Flow5
Fluidic Flow Control Devices for Gust Load Alleviation5
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus5
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale5
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers5
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging5
Experimental and Computational Investigation of Rotor Noise in Hover5
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary5
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering5
Machine Learning Models for Multirotor Performance Prediction4
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow4
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft4
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water4
Ice Shape Convergence in Multistep Ice Accretion Simulations4
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method4
Control-Oriented Modeling for Flexible Aircraft4
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System4
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface4
Stability, Modes, and Dynamics of Stratospheric Airships Across the Entire Ascent-Descent Envelope4
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps4
Energy-Harvesting Performance of an Aircraft Propeller4
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions4
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model4
Physics-Based Surface Condition Discriminant for a Time-Efficient Roughness Model4
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis4
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor4
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes4
Announcements and Acknowledgments4
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes4
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X4
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel4
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion4
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection4
Annoyance Model Assessments of Urban Air Mobility Vehicle Operations4
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft4
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics4
Transonic Flutter Dips of the AGARD 445.6 Wing4
Development of the Aspirated Kiel Probe3
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation3
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids3
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D3
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core3
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective3
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing3
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows3
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles3
Autorotation-Based Descent with Trajectory Optimization3
On the Use of Artificial Ice Shapes for Large-Eddy Simulations in Aircraft Icing3
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data3
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies3
Benefits and Challenges of Electric Propulsion for Commuter Aircraft3
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport3
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation3
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics3
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles3
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage3
Estimating Aircraft Landing Weights from Mode S Data3
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model3
Insights and Lessons Learned from the NASA Juncture Flow Experiment3
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings3
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions3
Effect of Squeezing Force on Stress and Fatigue of Aircraft Riveted Joints2
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests2
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation2
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments2
Controlled Flow in a Serpentine Diffuser with a Cowl Inlet2
Polynomial Chaos Kriging Models for Uncertainty Quantification in High-Speed Flow Applications2
Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion2
Uncertainty Propagation of Optimal Hybrid-Electric Aircraft Designs in Scenario-Based Framework2
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks2
Introduction to the Fourth AIAA High-Lift Prediction Workshop Virtual Collection2
Improving Structural Test and Analysis Correlation Using Digital Image Correlation Boundary Measurements2
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion2
Debiased Multifidelity Approach to Surrogate Modeling in Aerospace Applications2
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data2
Lamination-Parameter-Based Mass Minimization of the Common Research Model Wing Using Sandwich Composites2
Advancements in the Theory and Practice of Flight Vehicle System Identification2
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics2
Understanding High-Speed Aeroelastic Stability of a Gimballed Proprotor2
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction2
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing2
Preliminary Design Criteria for Supersonic Biplane2
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration2
Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds2
Aerodynamic Characteristics of Unmanned Aerial Vehicle with Z-Shaped Folding Wings2
Correction: Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design2
Liquid Cooling Systems for Batteries of Electric Vertical Takeoff and Landing Aircraft2
Baseline Simulated Ship-Helicopter Operating Limits for the NATO Generic Destroyer2
Efficient Aerostructural Wing Optimization Considering Mission Analysis2
Aerodynamic Design of Prop-Rotor Blades Using Neural Networks2
Quantifying Impacts of Uncertainties on Certification-Driven Design2
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter2
End-to-End Uncertainty Quantification with Analytical Derivatives for Design Under Uncertainty1
Dynamic Stability of the Hybrid Airship Influenced by Added Mass Effect1
Airfoil Morphed Leading-Edge Design for High-Lift Applications Using Genetic Algorithm1
Thermal Insulation Properties and Thermomechanical Properties of Metallic Thermal Protection Structure1
Coupled Aeropropulsive Design Optimization of an Over-wing Nacelle Configuration1
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap1
Flow Pattern of Compressible Convex-Corner Flow1
Integration of Uncertainty Quantification in a Model-Based Systems Analysis and Engineering Framework1
Multifidelity Design of Structurally Embedded Waveguides1
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact1
Design of Hybrid-Laminar-Flow-Control Wing and Suction System for Transonic Midrange Aircraft1
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
Nonlinear Multibody Modeling of Flexible Aircraft with Flared Hinged Wingtips1
Assessing the Feasibility of Hydrogen-Powered Aircraft: A Comparative Economic and Environmental Analysis1
Reynolds-Averaged Studies of the Sandia Transonic Bump Validation Challenge, with Loss of Symmetry1
Comparative Research on Landing and Rollout Characteristics of Skid-Equipped and Wheeled Aircraft1
Optimal Mission Profile for Low-Boom Supersonic Aircraft1
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data1
Design and Aerodynamic Analysis of Leading Edge for Morphing Wing1
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft1
Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System1
Propeller Ceiling Effect in Forward Flight1
Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling1
High Crosswind-Tolerance Airplane by Adjusting Dihedral Angle and Vertical Tail Volume1
Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification1
Fountain Flow Visualization in Quadrotor Wake Decreasing Rotor Thrust In-Ground Effect1
Scale Resolving Simulation of Buffet Effects Induced by Ultrahigh Bypass Ratio Nacelle Installation1
System Identification of Unmanned Air Systems at Texas A&M University1
Effect of Angle of Attack on Propeller Aeroacoustics at Positive and Negative Thrust1
Tiltwing eVTOL Transition Trajectory Optimization1
Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft1
About the Wing and Whirl Flutter of a Slender Wing–Propeller System1
Overview of System Identification Tool Advancements at Systems Technology, Incorporated1
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
Robust Optimization of a Thermal Anti-Ice Protection System in Uncertain Cloud Conditions1
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics1
Off-Design Performance Analysis of a Parallel Hybrid Electric Regional Turboprop Aircraft1
Numerical Simulation of the Flow in the ONERA F1 Wind Tunnel1
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America1
Retrofit Measures for Aircraft Noise Reduction: Simulation Benchmark and Impact Assessment1
Method for Quantifying Pollutant Emissions Within Preliminary Design of Small Aircraft1
Active Hinged Wingtip Control for Reducing Wing Root Bending Moment1
Deterministic and Probabilistic Approaches to Model and Update Dynamic Systems1
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control1
Stability of Gossamer Propellers for High-Altitude Ballooning1
Airfoil Separation Constraint Formulation for Aerodynamic Shape Optimization1
Study on the Anti-Icing of Conical Rotating Spinners with Different Cone Angles1
Letter from the Editor1
Estimation of the Fan Rotational Speed Using Flyover Audio Recordings1
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet1
Flutter Calculations Using the Unsteady Source and Doublet Panel Method1
Integrated Three-Dimensional Airloads and Stresses on Lift-Offset Coaxial Rotors at Extreme Speeds1
Aeropropulsive Shape Optimization of an Airfoil System in the Transonic Regime1
Transonic Shock Buffet Flowfield Assessment Using Various Dynamic Mode Decomposition Techniques1
Exploration of a Low-Speed, Flapped, Slotted, Natural-Laminar-Flow Airfoil1
Experimental Nonlinear Modal Analysis of an F-16 Aircraft Using Phase-Locked Loop Control1
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming1
Quality-Informed Test Design for Wind Tunnel Testing1
Numerical Modeling of Aircraft Fire: Postcrash Fire1
Numerical Investigation of Ice Formation on a Wing with Leading-Edge Tubercles1
Statistical Approach for Electric Taxiing Requirements for Regional Turboprop Aircraft1
Aircraft Parameter Estimation Considering Process and Measurement Noise1
Assessment of Aerodynamic Torque on Propeller Whirl Flutter and Its Control1
Low-Order Modeling of Stacked Rotor Performance in Hover1
Statistical Analysis of the Surface Roughness on Aircraft Icing1
Eigenvalue Sensitivity Computations for Linear Stability Theory1
Experimental Results for a Low-Reynolds-Number Airfoil in a Low-Turbulence Wind Tunnel1
Laminar–Turbulent Transition Prediction on Industrial Computational Fluid Dynamics Applications1
Results from the Second Ice Prediction Workshop by Using the CIRA Cartesian Method1
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