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 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
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion16
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
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
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
System Identification of a Subscale Distributed Electric Propulsion Aircraft12
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
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings11
Preliminary Design of a Drive System for a Midsized Coaxial Rotorcraft11
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts10
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport10
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
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
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters8
Efficient Algorithm of Real-Time Failure Probability Function Updating8
Development of Three-Dimensional Feature-Based Vision Algorithm for Ship-Deck Landing8
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
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
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
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
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
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
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
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes4
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
Transonic Flutter Dips of the AGARD 445.6 Wing4
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
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics4
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
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
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface4
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
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
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
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