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 2021-09-01 to 2025-09-01.)
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 Scales18
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion18
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data17
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition17
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 Active Flow Control over a Cranked-Delta Wing16
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft14
Effect of Partial Ground and Partial Ceiling on Propeller Performance14
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection13
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft13
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft12
System Identification of a Subscale Distributed Electric Propulsion Aircraft12
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance12
Advances in Aircraft System Identification at NASA Langley Research Center12
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport11
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels11
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft11
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings10
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling10
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts10
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems10
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions9
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters9
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization9
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing9
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage8
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads8
Interaction Between a Hovering Maritime Helicopter and Ship Exhaust Plume8
Efficient Algorithm of Real-Time Failure Probability Function Updating8
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio7
Investigation on “Replacing Bolts with Rivets” in Composite Structures7
Economic Aspects of Aircraft Propulsion Electrification7
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover7
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning7
Wind Tunnel Testing of Tethered Inflatable Wings7
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research7
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers7
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification7
Fixed-Time Trajectory Tracking Control for Airships with Time-Varying Error Constraints7
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data7
Flight-Test Determination of Longitudinal Stability Using System Identification7
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints6
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft6
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers6
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results6
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions6
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale6
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method6
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft6
Gust Response Predictions of a Very Flexible Wing Model6
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary6
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”6
Numerical Simulation of the Common Research Model with Natural Laminar Flow5
Multicomponent and Multifailure Mode Reliability Analysis of Rear Variable-Area Bypass Injector5
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft5
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV5
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering5
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design5
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes5
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps5
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging5
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method5
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus5
Fluidic Flow Control Devices for Gust Load Alleviation5
Experimental and Computational Investigation of Rotor Noise in Hover5
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X4
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions4
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics4
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection4
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft4
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis4
Ice Shape Convergence in Multistep Ice Accretion Simulations4
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface4
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel4
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow4
Announcements and Acknowledgments4
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System4
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows4
Machine Learning Models for Multirotor Performance Prediction4
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion4
Force Decoupling for Assembly Interface of Large Aircraft Structures by Neural Networks4
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water4
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes4
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics4
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor4
Physics-Based Surface Condition Discriminant for a Time-Efficient Roughness Model4
Control-Oriented Modeling for Flexible Aircraft4
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model4
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions4
Transonic Flutter Dips of the AGARD 445.6 Wing4
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method4
Energy-Harvesting Performance of an Aircraft Propeller4
Annoyance Model Assessments of Urban Air Mobility Vehicle Operations4
Stability, Modes, and Dynamics of Stratospheric Airships Across the Entire Ascent-Descent Envelope4
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage3
Development of the Aspirated Kiel Probe3
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles3
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data3
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective3
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model3
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation3
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation3
Autorotation-Based Descent with Trajectory Optimization3
On the Use of Artificial Ice Shapes for Large-Eddy Simulations in Aircraft Icing3
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings3
Aerodynamic Characteristics of Unmanned Aerial Vehicle with Z-Shaped Folding Wings3
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core3
Combined Flow Control Method for Supersonic Jet Noise Reduction3
Insights and Lessons Learned from the NASA Juncture Flow Experiment3
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids3
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles3
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing3
Estimating Aircraft Landing Weights from Mode S Data3
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments3
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies3
Outlier Detection for Distributed Pressure Measurements3
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D3
Effect of Squeezing Force on Stress and Fatigue of Aircraft Riveted Joints2
Benefits and Challenges of Electric Propulsion for Commuter Aircraft2
Geometric Deep Learning for Loads Prediction of Maneuvering Aircraft2
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data2
Controlled Flow in a Serpentine Diffuser with a Cowl Inlet2
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks2
Polynomial Chaos Kriging Models for Uncertainty Quantification in High-Speed Flow Applications2
Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion2
Quantifying Impacts of Uncertainties on Certification-Driven Design2
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing2
Improving Structural Test and Analysis Correlation Using Digital Image Correlation Boundary Measurements2
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration2
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport2
Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds2
Preliminary Design Criteria for Supersonic Biplane2
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter2
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction2
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics2
Liquid Cooling Systems for Batteries of Electric Vertical Takeoff and Landing Aircraft2
Introduction to the Fourth AIAA High-Lift Prediction Workshop Virtual Collection2
Understanding High-Speed Aeroelastic Stability of a Gimballed Proprotor2
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion2
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests2
Lamination-Parameter-Based Mass Minimization of the Common Research Model Wing Using Sandwich Composites2
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation2
Debiased Multifidelity Approach to Surrogate Modeling in Aerospace Applications2
Correction: Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design2
Uncertainty Propagation of Optimal Hybrid-Electric Aircraft Designs in Scenario-Based Framework2
Baseline Simulated Ship-Helicopter Operating Limits for the NATO Generic Destroyer2
Aerodynamic Design of Prop-Rotor Blades Using Neural Networks2
Advancements in the Theory and Practice of Flight Vehicle System Identification2
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America1
Novel Model-Based-Systems-Engineering-Driven Design Method for Aviation Electric Fuel Pump1
Stability Derivatives Prediction Using Reduced-Order Models on Triple Delta Wing1
Method for Quantifying Pollutant Emissions Within Preliminary Design of Small Aircraft1
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data1
Nonlinear Multibody Modeling of Flexible Aircraft with Flared Hinged Wingtips1
Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet1
Thermal Insulation Properties and Thermomechanical Properties of Metallic Thermal Protection Structure1
Integrated Three-Dimensional Airloads and Stresses on Lift-Offset Coaxial Rotors at Extreme Speeds1
Experimental Nonlinear Modal Analysis of an F-16 Aircraft Using Phase-Locked Loop Control1
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft1
Propeller Ceiling Effect in Forward Flight1
Numerical Simulation of the Flow in the ONERA F1 Wind Tunnel1
Flutter Calculations Using the Unsteady Source and Doublet Panel Method1
Quality-Informed Test Design for Wind Tunnel Testing1
Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification1
High Crosswind-Tolerance Airplane by Adjusting Dihedral Angle and Vertical Tail Volume1
Application of Mass Particle Methods in the Shape Design for Scientific Balloons1
Off-Design Performance Analysis of a Parallel Hybrid Electric Regional Turboprop Aircraft1
Tiltwing eVTOL Transition Trajectory Optimization1
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
Conceptual Design and Energy Management Analysis of Turbofan-Based Hybrid-Electric Propulsion1
Comparative Research on Landing and Rollout Characteristics of Skid-Equipped and Wheeled Aircraft1
Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft1
Effect of Angle of Attack on Propeller Aeroacoustics at Positive and Negative Thrust1
Optimal Mission Profile for Low-Boom Supersonic Aircraft1
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact1
Aeropropulsive Shape Optimization of an Airfoil System in the Transonic Regime1
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics1
Mixed H2/H∞ Control for Autonomous Quadrotor Landing via Linear Matrix Inequality Optimization1
Unsteady Effects of Blowing over Actuated Surfaces Using Phase-Locked Particle Image Velocimetry1
Integration of Uncertainty Quantification in a Model-Based Systems Analysis and Engineering Framework1
Transonic Shock Buffet Flowfield Assessment Using Various Dynamic Mode Decomposition Techniques1
Experimental Results for a Low-Reynolds-Number Airfoil in a Low-Turbulence Wind Tunnel1
Deterministic and Probabilistic Approaches to Model and Update Dynamic Systems1
Active Hinged Wingtip Control for Reducing Wing Root Bending Moment1
Study on the Anti-Icing of Conical Rotating Spinners with Different Cone Angles1
Design of Hybrid-Laminar-Flow-Control Wing and Suction System for Transonic Midrange Aircraft1
Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling1
Airfoil Separation Constraint Formulation for Aerodynamic Shape Optimization1
About the Wing and Whirl Flutter of a Slender Wing–Propeller System1
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap1
Airfoil Morphed Leading-Edge Design for High-Lift Applications Using Genetic Algorithm1
Design and Aerodynamic Analysis of Leading Edge for Morphing Wing1
Nonlinear Dynamics of Nitinol-Enhanced Carbon-Fiber-Reinforced Polymer Beam-Rod in Subsonic Flow1
Fountain Flow Visualization in Quadrotor Wake Decreasing Rotor Thrust In-Ground Effect1
Stability of Gossamer Propellers for High-Altitude Ballooning1
Scale Resolving Simulation of Buffet Effects Induced by Ultrahigh Bypass Ratio Nacelle Installation1
Statistical Analysis of the Surface Roughness on Aircraft Icing1
Exploration of a Low-Speed, Flapped, Slotted, Natural-Laminar-Flow Airfoil1
Unsteady Propeller Wake Interference on Wing in Tractor Configuration at Low-Reynolds-Number Condition1
Effect of Squeezing Force on Crack Propagation Life of Lap Riveted Structures1
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming1
System Identification of Unmanned Air Systems at Texas A&M University1
Assessment of Aerodynamic Torque on Propeller Whirl Flutter and Its Control1
Statistical Approach for Electric Taxiing Requirements for Regional Turboprop Aircraft1
Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling1
Low-Order Modeling of Stacked Rotor Performance in Hover1
Flow Pattern of Compressible Convex-Corner Flow1
Multifidelity Design of Structurally Embedded Waveguides1
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control1
Laminar–Turbulent Transition Prediction on Industrial Computational Fluid Dynamics Applications1
Numerical Investigation of High-Lift Propeller Positions for a Distributed Propulsion System1
Results from the Second Ice Prediction Workshop by Using the CIRA Cartesian Method1
Design Exploration of a Distributed Electric Propulsion Aircraft Using Explainable Surrogate Models1
Dynamic Stability of the Hybrid Airship Influenced by Added Mass Effect1
End-to-End Uncertainty Quantification with Analytical Derivatives for Design Under Uncertainty1
Retrofit Measures for Aircraft Noise Reduction: Simulation Benchmark and Impact Assessment1
Estimation of the Fan Rotational Speed Using Flyover Audio Recordings1
Letter from the Editor1
Numerical Investigation of Ice Formation on a Wing with Leading-Edge Tubercles1
Numerical Modeling of Aircraft Fire: Postcrash Fire1
Coupled Aeropropulsive Design Optimization of an Over-wing Nacelle Configuration1
Aircraft Parameter Estimation Considering Process and Measurement Noise1
Efficient Aerostructural Wing Optimization Considering Mission Analysis1
Robust Optimization of a Thermal Anti-Ice Protection System in Uncertain Cloud Conditions1
Overview of System Identification Tool Advancements at Systems Technology, Incorporated1
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