Journal of Aircraft

Papers
(The TQCC of Journal of Aircraft is 3. 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 2022-05-01 to 2026-05-01.)
ArticleCitations
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales31
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips31
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft30
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition29
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing27
Slipstream Deformation in Propeller–Wing–Flap Aerodynamic Interaction26
Energy Consumption of Airplane with New Propulsion Systems and Energy Carriers25
Determination of Mission Failure for Propeller-Driven High-Altitude, Long-Endurance UAVs Under Icing Conditions24
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail24
Effect of Partial Ground and Partial Ceiling on Propeller Performance21
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration21
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion21
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data19
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection18
Adap-Informer: An Adaptive Framework for Aircraft Fuel Prediction18
Effectiveness of Wing Morphing Techniques for Maneuverability: A Direct Comparison Method18
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data18
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft17
Advances in Aircraft System Identification at NASA Langley Research Center16
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings16
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft15
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport15
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels15
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts15
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions14
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling14
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance14
System Identification of a Subscale Distributed Electric Propulsion Aircraft14
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft14
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems14
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization13
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage13
Interaction Between a Hovering Maritime Helicopter and Ship Exhaust Plume12
Investigation on “Replacing Bolts with Rivets” in Composite Structures12
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio12
Data-Driven Complex Icing Scaling via Fused Super-Resolution Network12
Efficient Algorithm of Real-Time Failure Probability Function Updating12
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification11
Fixed-Time Trajectory Tracking Control for Airships with Time-Varying Error Constraints11
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning11
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing11
Individual Propeller Source Noise Assessment from Full-Scale eVTOL Flight Test Measurements11
Wind Tunnel Testing of Tethered Inflatable Wings10
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters10
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions10
Aeropropulsive Damping Characterization for eVTOL Aircraft Using Free-Motion Wind-Tunnel Testing10
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads10
Geopolitical Risk and Airline Stocks: Driver or Drag?10
Automatic Judging for Precision Aerobatics9
Gust Response Predictions of a Very Flexible Wing Model9
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft9
Aerodynamic Characteristics of Flat-Plate Delta Wing with Deflected Wing Tips9
Economic Aspects of Aircraft Propulsion Electrification9
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research9
Immersed Boundary Methodology for Three-Dimensional Multistep Ice Accretion Simulations9
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints9
Inlet Ground Vortex Investigation and Effect of Numerical Modeling strategies9
Coupling Dynamic Stall with Lifting-Line Theory for Gust and Maneuver Analysis9
Experimental Investigations of an Aeroelastic Wind Tunnel Model for Tail Buffeting Analysis9
Experimental Assessment of the Sprayed Liquid Flap9
Load Case and Constraint Downselection for Structural Optimization8
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results8
Comparison of Unmanned Aerial Vehicle Propeller Performance Under Atmospheric Ice Accretion8
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers8
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes8
Near-Terrain Flight Operations and Performance of Unmanned Aerial Vehicles8
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft8
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover8
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data8
Multicomponent and Multifailure Mode Reliability Analysis of Rear Variable-Area Bypass Injector8
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers8
Hybrid Powertrain Systems for 100 kg Multicopters and Tailsitters8
Flight-Test Determination of Longitudinal Stability Using System Identification8
Impact of Failure on the Tilt-Wing eVTOL Backward Transition8
Aerodynamic Interaction of a Boundary-Layer-Ingesting Propeller with a Fuselage Aft-Cone8
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging8
Performance Degradation and Ice Prediction in Rotating Blades: Experimental and Numerical Review8
Fluidic Flow Control Devices for Gust Load Alleviation7
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV7
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method7
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft7
Aerodynamic Optimization of a Three-Dimensional High-Lift System Considering Mechanical Feasibility7
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”7
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering7
Experimental and Computational Investigation of Rotor Noise in Hover7
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus7
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale7
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method7
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design7
Numerical Simulation of the Common Research Model with Natural Laminar Flow7
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps7
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary7
What Price Hover?6
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics6
Announcements and Acknowledgments6
Machine Learning Models for Multirotor Performance Prediction6
Control-Oriented Modeling for Flexible Aircraft6
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow6
Optimization of Aircraft Control Stick Force Using Bio-Inspired Swarm Intelligence Algorithms6
Applicability of Quadratic Constitutive Relations for Turbulent Flow Simulations in Aeronautics6
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes6
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft6
Analysis of Structural Flexibility Effects on Handling Qualities Using Variable Stability Simulations6
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X6
Enabling Interaction-Free Continuous Descent Through Eligible Flight Identification and Top-of-Descent Prediction6
Experimental Evaluation of the ASWING Aeroelastic Framework: Aeroelasticity Model6
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion6
Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles6
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel6
Stability, Modes, and Dynamics of Stratospheric Airships Across the Entire Ascent-Descent Envelope6
Range Estimation of Electric Aircraft with Dynamically Dissipated Energy and Constant Power5
Energy-Harvesting Performance of an Aircraft Propeller5
Impact of Takeoff Trajectory Design on Performance and Noise for Advanced Air Mobility Aircraft5
Development of the Aspirated Kiel Probe5
Correlations for Mean Properties of Turbulent Supersonic Flow over an Insulated Flat Plate5
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions5
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water5
Transonic Flutter Dips of the AGARD 445.6 Wing5
Annoyance Model Assessments of Urban Air Mobility Vehicle Operations5
Ice Shape Convergence in Multistep Ice Accretion Simulations5
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor5
Experimental Evaluation of the ASWING Aeroelastic Framework: Aerodynamics and Propeller Models5
Deep Iterative Convergence of Reynolds-Averaged Navier–Stokes Methods for High-Lift Aircraft Geometries5
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System5
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection5
Analysis of Wing Section Circulation Control Jet Bistability at Transonic Speeds5
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method5
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis5
Physics-Based Surface Condition Discriminant for a Time-Efficient Roughness Model5
Force Decoupling for Assembly Interface of Large Aircraft Structures by Neural Networks5
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions5
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface5
Outlier Detection for Distributed Pressure Measurements4
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation4
Determination of Acceptance Criteria for Aircraft Wet-Molding Composite Materials’ Void Content4
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows4
On the Use of Artificial Ice Shapes for Large-Eddy Simulations in Aircraft Icing4
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model4
Estimating Aircraft Landing Weights from Mode S Data4
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D4
Combined Flow Control Method for Supersonic Jet Noise Reduction4
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles4
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics4
Flight Demonstration and Model Validation of a Prototype Variable-Altitude Venus Aerobot4
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data4
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation4
Tiltrotor Whirl Flutter Mitigation Through Active Mini-Tab Control4
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage4
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles4
Aeroelastic Effects on a High-Aspect-Ratio Wing with Load Alleviation4
Ice Printer: Novel Method for Generating Impact Ice4
Design and Fleet Assessment of Commercial Aircraft with Range and Speed Optimization3
Baseline Simulated Ship-Helicopter Operating Limits for the NATO Generic Destroyer3
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing3
Analysis and Measurements of a Simulated Atmospheric Boundary Layer Using Cowdrey Rods3
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests3
Controlled Flow in a Serpentine Diffuser with a Cowl Inlet3
Aeroacoustic Study of Strut Braced Ultra-High Aspect Ratio Wings3
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion3
Effect of Squeezing Force on Stress and Fatigue of Aircraft Riveted Joints3
Fatigue of 1.5 Single-Shear Lap Joints with Sealant and Corrosion-Inhibiting Compounds3
Topology-Optimized Impact-Resistant Bionic Landing Gear for Unmanned Aerial Vehicles3
Insights and Lessons Learned from the NASA Juncture Flow Experiment3
Hybrid Solid-Oxide-Fuel-Cell-Powered Midrange Commercial Aircraft Concept3
Aeroengine Gas-Path Fault Diagnosis Based on Lightweight Dual-Stream Adaptive Lightweight Attention Network3
Aerodynamic Characteristics of Unmanned Aerial Vehicle with Z-Shaped Folding Wings3
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings3
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments3
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics3
Autorotation-Based Descent with Trajectory Optimization3
Aerodynamic Design of Prop-Rotor Blades Using Neural Networks3
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies3
Aerodynamic Characteristics of Laminar Airfoils with Oscillating Flaps: Experimental and Numerical Study3
Adaptive Model-Informed Controller for Tiltrotor Aircraft3
Historical Trends and Future Projections of Key Performance Parameters in Aircraft Design3
Advancements in the Theory and Practice of Flight Vehicle System Identification3
Correction: Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design3
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data3
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter3
Geometric Deep Learning for Loads Prediction of Maneuvering Aircraft3
Krueger Flap and Ultra-High-Bypass-Ratio Through-Flow Nacelle Design for the High-Lift Common Research Model3
Weight Estimation and Architecture Definition of Fuel Systems for Aircraft Conceptual Design3
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation3
Improving Structural Test and Analysis Correlation Using Digital Image Correlation Boundary Measurements3
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core3
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks3
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids3
Quantifying Impacts of Uncertainties on Certification-Driven Design3
Lamination-Parameter-Based Mass Minimization of the Common Research Model Wing Using Sandwich Composites3
Preliminary Design Criteria for Supersonic Biplane3
Introduction to the Fourth AIAA High-Lift Prediction Workshop Virtual Collection3
Efficient Algorithm for Estimating Generalized Failure Probability Function of Aeroengine Turboshafts3
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing3
Physical Characteristics of Leading-Edge Vortices of a Delta Wing at Sideslip3
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective3
Debiased Multifidelity Approach to Surrogate Modeling in Aerospace Applications3
Benefits and Challenges of Electric Propulsion for Commuter Aircraft3
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model3
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport3
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration3
0.10519790649414