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 2022-01-01 to 2026-01-01.)
ArticleCitations
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips30
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales23
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft22
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion22
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration21
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data21
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail20
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing18
Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition18
Slipstream Deformation in Propeller–Wing–Flap Aerodynamic Interaction18
Energy Consumption of Airplane with New Propulsion Systems and Energy Carriers16
Determination of Mission Failure for Propeller-Driven High-Altitude, Long-Endurance UAVs Under Icing Conditions16
Effect of Partial Ground and Partial Ceiling on Propeller Performance16
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data15
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling14
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft14
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts14
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft13
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels13
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings13
System Identification of a Subscale Distributed Electric Propulsion Aircraft13
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection13
Advances in Aircraft System Identification at NASA Langley Research Center12
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance12
Aerodynamic Nonlinear Modeling and Body-Freedom Flutter Suppression of Flying-Wing Aircraft12
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization12
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport12
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems11
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters11
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions11
Investigation on “Replacing Bolts with Rivets” in Composite Structures10
Aerodynamic Characteristics of Magnetically Suspended Square Cylinders with Low Fineness Ratio10
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage10
Aeropropulsive Damping Characterization for eVTOL Aircraft Using Free-Motion Wind-Tunnel Testing10
Nonintrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification9
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads9
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning9
Geopolitical Risk and Airline Stocks: Driver or Drag?9
Interaction Between a Hovering Maritime Helicopter and Ship Exhaust Plume9
Wind Tunnel Testing of Tethered Inflatable Wings9
Efficient Algorithm of Real-Time Failure Probability Function Updating9
Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft8
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing8
Parametric Study of a Switchable Vortex Generator for Load Alleviation in Transonic Conditions8
Brake-Induced Landing Gear Walk Vibration Analysis and Suppression Method Research8
Gust Response Predictions of a Very Flexible Wing Model8
Fixed-Time Trajectory Tracking Control for Airships with Time-Varying Error Constraints8
Impact of Failure on the Tilt-Wing eVTOL Backward Transition8
Comparison of Unmanned Aerial Vehicle Propeller Performance Under Atmospheric Ice Accretion8
Data-Driven Complex Icing Scaling via Fused Super-Resolution Network8
Economic Aspects of Aircraft Propulsion Electrification8
Phase-Resolved Flowfield Measurements of a Coaxial Counter-Rotating Rotor in Hover7
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints7
Inlet Ground Vortex Investigation and Effect of Numerical Modeling strategies7
Optimal Range and Endurance for Electric Aircraft Driven by Fixed-Pitch Propellers7
Numerical Icing Simulations of Cylindrical Geometry and Comparisons to Flight Test Results7
Automatic Judging for Precision Aerobatics7
Flight-Test Determination of Longitudinal Stability Using System Identification7
Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft7
Numerical Simulation of the Common Research Model with Natural Laminar Flow6
Comprehensive Review of Design and Performance Metrics in Three-Surface Aircraft6
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design6
Note on the Non-CO2 Mitigation Potential of Hybrid-Electric Aircraft Using “Eco-Switch”6
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale6
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus6
System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data6
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging6
Fluidic Flow Control Devices for Gust Load Alleviation6
Load Case and Constraint Downselection for Structural Optimization6
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers6
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV6
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method6
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes6
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics5
Multicomponent and Multifailure Mode Reliability Analysis of Rear Variable-Area Bypass Injector5
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary5
Near-Terrain Flight Operations and Performance of Unmanned Aerial Vehicles5
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps5
Modeling of the Six-Degree-of-Freedom Nonlinear Ground Dynamics of the Cessna Citation X5
Machine Learning Models for Multirotor Performance Prediction5
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel5
Announcements and Acknowledgments5
Performance Degradation and Ice Prediction in Rotating Blades: Experimental and Numerical Review5
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface5
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method5
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering5
Application of Higher-Order Difference Schemes in Coupled Heat Transfer Simulation of Hypersonic Flow5
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis5
Physics-Based Surface Condition Discriminant for a Time-Efficient Roughness Model5
Annoyance Model Assessments of Urban Air Mobility Vehicle Operations5
Experimental Evaluation of the ASWING Aeroelastic Framework: Aeroelasticity Model5
What Price Hover?5
Experimental and Computational Investigation of Rotor Noise in Hover5
Aerodynamic Optimization of a Three-Dimensional High-Lift System Considering Mechanical Feasibility5
Hybrid Powertrain Systems for 100 kg Multicopters and Tailsitters5
Applicability of Quadratic Constitutive Relations for Turbulent Flow Simulations in Aeronautics5
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor5
Force Decoupling for Assembly Interface of Large Aircraft Structures by Neural Networks5
Stability, Modes, and Dynamics of Stratospheric Airships Across the Entire Ascent-Descent Envelope5
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes5
Aerodynamic Interaction of a Boundary-Layer-Ingesting Propeller with a Fuselage Aft-Cone5
Energy-Harvesting Performance of an Aircraft Propeller4
Transonic Flutter Dips of the AGARD 445.6 Wing4
Control-Oriented Modeling for Flexible Aircraft4
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water4
Correlations for Mean Properties of Turbulent Supersonic Flow over an Insulated Flat Plate4
On the Use of Artificial Ice Shapes for Large-Eddy Simulations in Aircraft Icing4
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles4
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method4
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion4
Ice Shape Convergence in Multistep Ice Accretion Simulations4
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection4
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows4
Investigating the Effect of Engine Including Heat Propulsion Components on Airframe Aerodynamics4
Analysis of Structural Flexibility Effects on Handling Qualities Using Variable Stability Simulations4
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System4
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft4
Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles4
Impact of Takeoff Trajectory Design on Performance and Noise for Advanced Air Mobility Aircraft4
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions4
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions4
Flight Demonstration and Model Validation of a Prototype Variable-Altitude Venus Aerobot4
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core3
Aerodynamics of High-Bypass-Ratio Aeroengine Nacelles: Numerical and Experimental Investigation3
Estimating Aircraft Landing Weights from Mode S Data3
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D3
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings3
Aeroelastic Effects on a High-Aspect-Ratio Wing with Load Alleviation3
Development of the Aspirated Kiel Probe3
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model3
Geometric Deep Learning for Loads Prediction of Maneuvering Aircraft3
Large-Eddy Simulation of Wake Vortices at Tokyo/Haneda International Airport3
Design Optimization of Lambda-Wing Planform and Vortex Generators for Longitudinal Instability Alleviation3
Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies3
HEMLAB Algorithm Applied to the High-Lift Japan Aerospace Exploration Agency Standard Model3
MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids3
Autorotation-Based Descent with Trajectory Optimization3
Deep Iterative Convergence of Reynolds-Averaged Navier–Stokes Methods for High-Lift Aircraft Geometries3
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles3
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing3
Ice Printer: Novel Method for Generating Impact Ice3
Debiased Multifidelity Approach to Surrogate Modeling in Aerospace Applications3
Benefits and Challenges of Electric Propulsion for Commuter Aircraft3
Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective3
Insights and Lessons Learned from the NASA Juncture Flow Experiment3
Tiltrotor Whirl Flutter Mitigation Through Active Mini-Tab Control3
Fretting Fatigue of Riveted Lap Joints in Aircraft Fuselage3
Combined Flow Control Method for Supersonic Jet Noise Reduction3
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation3
Outlier Detection for Distributed Pressure Measurements3
Nonlinear Aero-Propulsive Modeling for Fixed-Wing eVTOL UAV from Flight Test Data3
Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data3
Investigation of Energy-Maneuverability Methods for Helicopter Performance Assessments3
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