Journal of Aircraft

Papers
(The TQCC of Journal of Aircraft is 4. 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 2022-08-01 to 2026-08-01.)
ArticleCitations
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips38
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales35
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft35
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail31
Adap-Informer: An Adaptive Framework for Aircraft Fuel Prediction31
Determination of Mission Failure for Propeller-Driven High-Altitude, Long-Endurance UAVs Under Icing Conditions31
Effect of Partial Ground and Partial Ceiling on Propeller Performance31
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration29
Energy Consumption of Airplane with New Propulsion Systems and Energy Carriers26
Slipstream Deformation in Propeller–Wing–Flap Aerodynamic Interaction25
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data24
Effectiveness of Wing Morphing Techniques for Maneuverability: A Direct Comparison Method23
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion23
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing22
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data22
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition21
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection20
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts20
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling19
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport19
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft19
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions18
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft17
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance17
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels17
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft16
Improvements to the Medida–Baeder Transition Model for Three-Dimensional Transonic Flows16
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization16
System Identification of a Subscale Distributed Electric Propulsion Aircraft15
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings15
Advances in Aircraft System Identification at NASA Langley Research Center15
Aeroacoustic Study of a Generic Nose Landing Gear Focusing on Steering Mechanism15
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems14
Data-Driven Complex Icing Scaling via Fused Super-Resolution Network14
Multiple Trim Solutions Assessment for a Bio-Inspired Rotating Empennage Fighter Aircraft14
Aerodynamic Performance of Camber-Morphing Airfoils in Transonic and Supersonic Flow14
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage14
Interaction Between a Hovering Maritime Helicopter and Ship Exhaust Plume13
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification13
Efficient Algorithm of Real-Time Failure Probability Function Updating13
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads13
Investigation on “Replacing Bolts with Rivets” in Composite Structures13
Wind Tunnel Testing of Tethered Inflatable Wings13
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing12
Individual Propeller Source Noise Assessment from Full-Scale eVTOL Flight Test Measurements12
Fixed-Time Trajectory Tracking Control for Airships with Time-Varying Error Constraints12
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning12
Aerodynamic Characteristics of Flat-Plate Delta Wing with Deflected Wing Tips11
Geopolitical Risk and Airline Stocks: Driver or Drag?11
Aeropropulsive Damping Characterization for eVTOL Aircraft Using Free-Motion Wind-Tunnel Testing11
Immersed Boundary Methodology for Three-Dimensional Multistep Ice Accretion Simulations11
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio11
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters11
Coupling Dynamic Stall with Lifting-Line Theory for Gust and Maneuver Analysis11
Optimization of Net Deployment Performance in Two-Stage Ejection for UAV Capture11
Experimental Investigations of an Aeroelastic Wind Tunnel Model for Tail Buffeting Analysis10
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover10
Automatic Judging for Precision Aerobatics10
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft10
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft10
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints10
Economic Aspects of Aircraft Propulsion Electrification10
Experimental Assessment of the Sprayed Liquid Flap10
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions10
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data10
Gust Response Predictions of a Very Flexible Wing Model10
Inlet Ground Vortex Investigation and Effect of Numerical Modeling strategies10
Flight-Test Determination of Longitudinal Stability Using System Identification9
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers9
Comparison of Unmanned Aerial Vehicle Propeller Performance Under Atmospheric Ice Accretion9
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes9
Hybrid Powertrain Systems for 100 kg Multicopters and Tailsitters9
Impact of Failure on the Tilt-Wing eVTOL Backward Transition9
Study on a Pitching Natural-Laminar-Flow-0414 Airfoil at Low Reynolds Number9
Near-Terrain Flight Operations and Performance of Unmanned Aerial Vehicles9
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft9
Load Case and Constraint Downselection for Structural Optimization9
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research9
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results9
Aerodynamic Interaction of a Boundary-Layer-Ingesting Propeller with a Fuselage Aft-Cone9
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale9
Performance Degradation and Ice Prediction in Rotating Blades: Experimental and Numerical Review9
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging8
Deformation Analysis of Coated Aircraft Wing Using Fluid–Structure Interface8
Numerical Simulation of the Common Research Model with Natural Laminar Flow8
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”8
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method8
Crashworthiness Analysis and Design of Typical Aircraft Subcargo Fuselage Section8
Can Anisotropy Contribute to Tuning Thermal Expansion of Titanium Alloy Structures?8
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering8
Fluidic Flow Control Devices for Gust Load Alleviation8
Aerodynamic Optimization of a Three-Dimensional High-Lift System Considering Mechanical Feasibility8
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method8
Multicomponent and Multifailure Mode Reliability Analysis of Rear Variable-Area Bypass Injector8
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV8
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design8
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary8
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers8
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus8
Experimental and Computational Investigation of Rotor Noise in Hover8
Testing the High-Lift Common Research Model at the ONERA F1 Wind Tunnel8
Experimental Evaluation of the ASWING Aeroelastic Framework: Aeroelasticity Model7
What Price Hover?7
Numerical and Experimental Icing Simulations of the Next-Generation Civil Tiltrotor Engine Intake7
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps7
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow7
Enabling Interaction-Free Continuous Descent Through Eligible Flight Identification and Top-of-Descent Prediction7
Optimization of Aircraft Control Stick Force Using Bio-Inspired Swarm Intelligence Algorithms7
Stability, Modes, and Dynamics of Stratospheric Airships Across the Entire Ascent-Descent Envelope7
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X7
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel7
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis6
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes6
Force Decoupling for Assembly Interface of Large Aircraft Structures by Neural Networks6
Physics-Based Surface Condition Discriminant for a Time-Efficient Roughness Model6
Aerodynamic and Static Aeroelastic Analysis of a High-Agility Aircraft6
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion6
Analysis of Wing Section Circulation Control Jet Bistability at Transonic Speeds6
Applicability of Quadratic Constitutive Relations for Turbulent Flow Simulations in Aeronautics6
Control-Oriented Modeling for Flexible Aircraft6
Experimental Evaluation of the ASWING Aeroelastic Framework: Aerodynamics and Propeller Models6
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface6
Transonic Flutter Dips of the AGARD 445.6 Wing6
Ice Shape Convergence in Multistep Ice Accretion Simulations6
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics6
Announcements and Acknowledgments6
Impact of Takeoff Trajectory Design on Performance and Noise for Advanced Air Mobility Aircraft6
Range Estimation of Electric Aircraft with Dynamically Dissipated Energy and Constant Power6
Energy-Harvesting Performance of an Aircraft Propeller6
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft6
Flutter Boundary Prediction Based on Feature Extraction and Bayesian Optimization Transformer–Long Short-Term Memory6
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics5
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows5
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water5
Machine Learning Models for Multirotor Performance Prediction5
Development of the Aspirated Kiel Probe5
Annoyance Model Assessments of Urban Air Mobility Vehicle Operations5
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing5
Deep Iterative Convergence of Reynolds-Averaged Navier–Stokes Methods for High-Lift Aircraft Geometries5
Flight Demonstration and Model Validation of a Prototype Variable-Altitude Venus Aerobot5
Aeroelastic Effects on a High-Aspect-Ratio Wing with Load Alleviation5
Correlations for Mean Properties of Turbulent Supersonic Flow over an Insulated Flat Plate5
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System5
Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles5
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method5
Evaluating Follower Wing Performance in Formation Flight Using the Power Balance Method5
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles5
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage5
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model5
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection5
Analysis of Structural Flexibility Effects on Handling Qualities Using Variable Stability Simulations5
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor5
On the Use of Artificial Ice Shapes for Large-Eddy Simulations in Aircraft Icing5
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions5
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles5
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions5
Aeroengine Gas-Path Fault Diagnosis Based on Lightweight Dual-Stream Adaptive Lightweight Attention Network4
Surface-Vorticity-Based Aeropropulsive Analysis of a Tandem Tiltwing Aircraft4
Geometric Deep Learning for Loads Prediction of Maneuvering Aircraft4
Ice Printer: Novel Method for Generating Impact Ice4
Aerodynamic Characteristics of Unmanned Aerial Vehicle with Z-Shaped Folding Wings4
Active Flow Control Applications to High-Lift Leading-Edge Devices4
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport4
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments4
Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds4
Design and Fleet Assessment of Commercial Aircraft with Range and Speed Optimization4
Effect of Squeezing Force on Stress and Fatigue of Aircraft Riveted Joints4
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation4
Weight Estimation and Architecture Definition of Fuel Systems for Aircraft Conceptual Design4
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D4
Hybrid Solid-Oxide-Fuel-Cell-Powered Midrange Commercial Aircraft Concept4
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective4
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings4
Lamination-Parameter-Based Mass Minimization of the Common Research Model Wing Using Sandwich Composites4
Outlier Detection for Distributed Pressure Measurements4
Flutter Boundary Prediction Method Based on Long Short-Term Memory Networks4
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies4
Benefits and Challenges of Electric Propulsion for Commuter Aircraft4
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model4
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation4
Performance-Oriented Supercritical Airfoil Sampling Method for Deep Learning and Geometry Predictions4
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration4
Combined Flow Control Method for Supersonic Jet Noise Reduction4
Influence of Fuel Tank Design on the Energy Demand of Hydrogen Aircraft4
Autorotation-Based Descent with Trajectory Optimization4
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests4
Aerothermoelastic Analysis and Topology Optimization Based on the Meshfree Method4
Determination of Acceptance Criteria for Aircraft Wet-Molding Composite Materials’ Void Content4
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data4
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data4
Krueger Flap and Ultra-High-Bypass-Ratio Through-Flow Nacelle Design for the High-Lift Common Research Model4
Tiltrotor Whirl Flutter Mitigation Through Active Mini-Tab Control4
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids4
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core4
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion4
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation4
Insights and Lessons Learned from the NASA Juncture Flow Experiment4
Estimating Aircraft Landing Weights from Mode S Data4
Debiased Multifidelity Approach to Surrogate Modeling in Aerospace Applications4
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