Journal of Aircraft

Papers
(The median citation count of Journal of Aircraft is 0. 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 2021-03-01 to 2025-03-01.)
ArticleCitations
Numerical Modeling of Aircraft Fire: Postcrash Fire12
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration12
Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling11
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion11
Potential for Energy Recovery from Boundary-Layer Ingesting Actuator Disk Propulsion11
Announcements and Acknowledgments10
Steady and Unsteady Hover Test of a Lift Compounding Rotorcraft9
Transonic Flutter Dips of the AGARD 445.6 Wing9
Assessment of Potential Commercial Success of Business Jets with Natural Laminar Flow8
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System8
2025 AIAA Journal of Aircraft Editorial7
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor7
Eigenvalue Sensitivity Computations for Linear Stability Theory7
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing7
Impact of Phase Offset on the Flowfields Downstream of Synchronized Propellers6
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft6
Implementation of Fuel-Saving Relaxed Climb Procedure6
Unsteady Propeller Wake Interference on Wing in Tractor Configuration at Low-Reynolds-Number Condition6
Exploration of a Low-Speed, Flapped, Slotted, Natural-Laminar-Flow Airfoil6
Evaluation of Unmanned Aerial Vehicle Swarm Design Through Metrics of Survivability6
An Enhanced Jig-Shape Approach to Lifting Propeller Design6
Optimal Mission Profile for Low-Boom Supersonic Aircraft5
Improvement of Icing Simulation with Novel Ice Crystal Sticking Model5
Transonic Corrections for the Unsteady Compressible Source and Doublet Panel Method5
Metamodeling Approach for Wing Structural Sizing of Box-Wing Aircraft5
Machine Learning Models for Multirotor Performance Prediction5
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method5
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales5
Minimum Trim Drag for a Three-Surface Supersonic Transport Aircraft5
Flow Control Devices for Aeroacoustic Noise Suppression in Cavity Flow5
Ice Shape Convergence in Multistep Ice Accretion Simulations5
Effect of Partial Ground and Partial Ceiling on Propeller Performance5
Design Exploration of Transonic Airfoils for Natural and Hybrid Laminar Flow Control Applications4
Plasma Gurney Flap Flight Control at Low Angle of Attack4
Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft4
High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring4
Structural Optimization of a Large-Scale 3D-Printed High-Altitude Propeller Blade with Experimental Validation4
HLPW-4: Wall-Modeled Large-Eddy Simulation and Lattice–Boltzmann Technology Focus Group Workshop Summary4
System Identification of Unmanned Air Systems at Texas A&M University4
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing4
Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data4
Overview of System Identification Tool Advancements at Systems Technology, Incorporated4
Control-Oriented Modeling for Flexible Aircraft4
Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft3
Induced-Strain Actuators for Morphing of Multi-Element Airfoils3
Investigation of Aerodynamic Support Interference for Testing a Semispan T Tail Aircraft Model3
Fluid–Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft3
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion3
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles3
Including Blade Elasticity into Frequency-Domain Propeller Whirl Flutter Analysis3
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes3
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface3
Piezoelectric-Actuator De-Icing Array Design Based on Structural Vibration Modes3
Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft3
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft3
Fleet Design Optimization of Package Delivery Unmanned Aerial Vehicles Considering Operations3
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming3
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water3
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail3
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact3
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis3
Comparison of Overwing and Underwing Nacelle Aeropropulsion Optimization for Subsonic Transport Aircraft3
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips3
Unsteady Effects of Blowing over Actuated Surfaces Using Phase-Locked Particle Image Velocimetry2
Experimental Results for a Low-Reynolds-Number Airfoil in a Low-Turbulence Wind Tunnel2
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection2
Conceptual Design of Aircraft System Routing Architectures Using a Bio-Inspired Algorithm2
Theodorsen’s and Garrick’s Flutter Calculations: Revisited2
Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation2
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection2
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport2
Three-Dimensional Aeromechanical Analysis of Lift Offset Coaxial Rotors: A Helios Test Case2
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control2
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling2
Correlation of High-Speed Tiltrotor Stability Predictions with Test Data and Parametric Study2
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft2
Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings2
Advances and Modern Applications of Frequency-Domain Aircraft and Rotorcraft System Identification2
Influence of Stitch Angle on the Flexural Response of Composite Structures2
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft2
Scale Effects in Wind Tunnel Testing: Extrapolation of the Drag Coefficient2
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts2
Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design2
Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing2
Macro- and Mesoscopic Design for Cabin Door Pretightened Fabric Rubber Seal Structure2
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization2
High-Fidelity Simulations of a Slotted, Natural-Laminar-Flow Wing Section2
Control Authority of a Single-Surface Parafoil with Bleed-Air Spoilers2
Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations2
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics2
Pseudospectral-Method-Based Framework for Rotorcraft Stability and Trim Analysis2
Experimental Assessment of the Poststall Performance of Two Highly Cambered Airfoils1
Prediction of Noise-Power-Distance Data for Urban Air Mobility Vehicles1
Integrated Three-Dimensional Airloads and Stresses on Lift-Offset Coaxial Rotors at Extreme Speeds1
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap1
Uncertainty Quantification of Laminar–Turbulent Transition on Airfoil and Fuselage1
Simulation and Regression Modeling of NASA’s X-59 Low-Boom Carpets Across America1
Individual Blade Control Approach for Active Vibration Suppression of a Lift-Offset Coaxial Rotorcraft1
Ducted Fan Design for VTOL Aircraft Flight Mission Based on Bayesian Optimization1
Numerical Analysis of Porpoising Stability Limit of a Blended-Wing–Body Aircraft During Ditching1
Automated Finite Element Analysis of Stiffened Tanks Using Multifidelity Modeling1
Multifidelity Rotor Wake Modeling with Uncertainty Quantification of Transitioning Tilt-Propeller Aircraft Performance1
Advances in Aircraft System Identification at NASA Langley Research Center1
DPW-7: Steady and Unsteady Computations of the Common Research Model at Different Reynolds Numbers1
Numerical Investigation into Single and Double Gurney Flaps for Improving Airfoil Performance1
Methodology for Preliminary Flight Control Actuator Design1
Integrated Design Optimization of Environmental Control Systems for Next-Generation Aircraft1
Analytical and Experimental Power Minimization for Fixed-Pitch Coaxial Rotors in Hover1
Unmanned Wingless Rotorcraft Scaling1
On the Effect of Geometric Nonlinearity on the Dynamics of Flared Folding Wingtips1
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows1
Research on Anti-Rollover Adaptive Landing Gear Technology Based on Impedance Control1
Nonlinear Dynamic Modeling for Aircraft with Unknown Mass Properties Using Flight Data1
Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification1
Aerodynamic Characterization of a Wind Tunnel Using Experimental and Computational Methods1
Energy-Based Aerodynamic Loss and Recovery Characteristics of Adiabatic and Heated Fuselages1
Optimal Performance Trim Procedure for Multirotor Vertical Takeoff and Landing Vehicles1
Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions1
Airfoil Design Framework for Optimized Boundary-Layer Integral Parameters1
Modification of the Class-Shape-Transformation Parameterization Based on Radial Basis Functions1
Reynolds-Averaged Studies of the Sandia Transonic Bump Validation Challenge, with Loss of Symmetry1
Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling1
Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics1
Multi-Objective Airfoil Optimization Under Unsteady-Freestream Dynamic Stall Conditions1
Trade-Space Assessment of Liquid Hydrogen Propulsion Systems for Electrified Aircraft1
Trajectory Optimization for Dynamic Soaring Remotely Piloted Aircraft with Under-Wing Solar Panels1
Flutter Calculations Using the Unsteady Source and Doublet Panel Method1
Remote Uncorrelated Pilot Input Excitation Assessment for Unmanned Aircraft Aerodynamic Modeling1
Optimization and Decision-Making Framework for Small Unmanned Aircraft Systems Fleet Design1
Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Using Large-Eddy Simulation1
Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design1
Aerodynamic Characteristics and Topology of Interfering Vortex Systems at Hybrid-Delta Wings1
Statistical Approach for Electric Taxiing Requirements for Regional Turboprop Aircraft1
Aerodynamic Exergy-Based Analysis and Optimization of the Generic Hypersonic Vehicle Using FUN3D1
Blended Wing Body Configuration for Hydrogen-Powered Aviation1
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration1
Potential for Energy Recovery of a Nonadiabatic Subsonic Airfoil1
Fast Nonlinear Static Aeroelasticity Method for High-Aspect-Ratio Wings at Different Mach Regimes1
Powered Low-Speed Experimental Aerodynamic Investigation of an Over-Wing-Mounted Nacelle Configuration1
Design of Rotary Wings with Passive Mitigation of Coherent Tip Vortex Roll-Up1
Aeropropulsive Shape Optimization of an Airfoil System in the Transonic Regime1
Correction: Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag1
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads1
Scoring Approach to Assess Maintenance Risk for Aircraft Systems in Conceptual Design1
Prediction of the Oswald Efficiency Factor for Cambered and Swept Wings1
Low-Order Modeling of Stacked Rotor Performance in Hover1
Design and Optimization of a Piecewise Flight Controller for VTOL UAVs1
Prediction of Hover Validation and Acoustic Baseline Hovering Rotor Performance and Ground Effect Using Mercury Framework1
System Identification of a Subscale Distributed Electric Propulsion Aircraft1
Development of an Aeromechanics Solver for Loads and Stability of Hingeless Tiltrotors1
Investigation on “Replacing Bolts with Rivets” in Composite Structures1
Drag Decomposition Using Partial-Pressure Fields: Ventus-3 and NASA Common Research Model1
Roll Maneuverability of Transonic High-Aspect-Ratio-Wing Aircraft with Flared Folding Wingtips1
Dynamic Model of Vapor Compression Systems for Aircraft Environmental Control Systems1
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning1
Numerical Investigation of Low-Noise Landing Conditions for Multirotor Urban Air Mobility Vehicle1
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft1
Planform Mesh Requirements for Fixed and Rotating Wing with Separation1
Autorotation-Based Descent with Trajectory Optimization1
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles1
Recent Applications of System Identification Techniques at IPEV1
Automatic Continuous Thrust Control for Supersonic Transport Takeoff Noise Reduction1
Three-Dimensional Spatial Atmospheric Turbulence Generation Method for Aerial Refueling Flight Simulation1
Towards Wall-Resolved Large-Eddy Simulation of the High-Lift Common Research Model1
Three-Dimensional Front-Tracking Technique for Multistep Simulations of Aircraft Icing1
Advancements in the Theory and Practice of Flight Vehicle System Identification0
Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle0
Coupled Aeropropulsive Design Optimization of an Over-wing Nacelle Configuration0
Sizing of High-Aspect-Ratio Wings with Folding Wingtips0
Real-Time Simulation of a Shipborne Rotor via Linearized State-Space Free-Vortex Wake Models0
Exploring Design Options for Wing Leading Edge Against Bird Strike0
Assessment of Added Masses Effects on Airship Dynamics and Stability0
Airfoil Flowfield Prediction Based on Proper Orthogonal Decomposition with Deep Learning0
On the Dynamic Behavior of Wings Incorporating Floating Wingtip Fuel Tanks0
Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method0
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction0
Study of Nonlinear Stiffness and Damping Effects on Shimmy and Flutter0
Efficient Aerostructural Wing Optimization Considering Mission Analysis0
Verification of the γ-Reθt Transition Model in OVERFLOW and FUN3D0
Turbulent Airwake Estimation from Helicopter–Ship Wind-Tunnel Data0
Freestream Turbulence Effects in Large-Eddy Simulations of Laminar Separation Bubble0
Optimal Design and Verifications of Cable-Suspension Mechanism for High-Angle-of-Attack Unsteady Tests0
In-Air Trapped Static Method for Aircraft Pressure Altitude and Airspeed0
Acoustic Liner Demonstrator for a Turning Vane of S1MA Wind Tunnel0
Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method0
Examination of End Plate Sizing for Reflection Plane Wind-Tunnel Testing0
Variable Noise Reduction Systems for a Notional Supersonic Business Jet0
Computational Evaluation of Turbo- and Electric-Powered Simulators for Turbofan Wind Tunnel Test0
Approach for Aerodynamic Gust Load Alleviation by Means of Spanwise-Segmented Flaps0
Influence of Nonlinear Static Deformation on the Pre-Pazy and Pazy Wing Flutter0
Experimental Study on a Liquid Hydrogen Tank for Unmanned Aerial Vehicle Applications0
Optimum Flap Deflection for Improved Aircraft Performance Using Surrogate Modeling0
Numerical Mach Number Studies on a Multidelta Wing Configuration with Vertical Stabilizers0
Load Reduction During Resonance Crossing of a Variable-Speed Rotor0
Deriving Lidar Sensor Requirements for Use in Wake Impact Alleviation Functions0
Letter from the Editor0
Unified Modeling of the TiltRotor Aeroelastic Stability Testbed for Proprotor Whirl Flutter0
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing0
Titanium Wind Tunnel Balance Leveraging Additive Manufacturing0
Flowfield of an S-Shaped Inlet with High Boundary-Layer Ingestion Fraction0
Aerodynamic Characteristics of Aircraft Model with Cable Suspension System under Rotary Motion0
On Improved Understanding of Airfoil Performance Evaluation Methods at Low Reynolds Numbers0
Airfoil Separation Constraint Formulation for Aerodynamic Shape Optimization0
Numerical Simulation of the High-Speed Leg of the National Transonic Facility0
Generation of Tow Paths on a Curved Shell in Three-Dimensional Space for Fiber Steering0
Impact of Airframe–Propulsion System Modeling Strategies on Key Structural Performance Metrics0
Aerodynamic Characteristics of Cruciform Parachute with an Asymmetric Configuration of Ropes0
Quantifying Impacts of Uncertainties on Certification-Driven Design0
Aerodynamic Optimization and Fuel Burn Evaluation of a Transonic Strut-Braced-Wing Single-Aisle Aircraft0
Passive Thermal Management of an Electric Trainer Aircraft Battery Pack Considering Aging0
Tiltwing eVTOL Transition Trajectory Optimization0
System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains0
Controlled Flow in a Serpentine Diffuser with a Cowl Inlet0
Compressor and Valve Control Performance Implications on Active Flow Control Aircraft0
Fluidic Flow Control Devices for Gust Load Alleviation0
Transonic Shock Buffet Flowfield Assessment Using Various Dynamic Mode Decomposition Techniques0
Improvement of Helicopter Operations on Frigates Using the Coanda Effect0
Experimental and Computational Investigation of Rotor Noise in Hover0
Steady Versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration0
Multifidelity Design of Structurally Embedded Waveguides0
Numerical Simulation of the Common Research Model with Natural Laminar Flow0
Modern Implementation and Evaluation of Lifting-Line Theory for Complex Geometries0
Methodology for Evaluating a Distributed Variable-Camber Trailing-Edge System in Preliminary Aircraft Design0
Simple Rules for Parachute Inflation Testing at Underscale and Performance Extrapolation to Full-Scale0
Modeling and Dynamic Stability Analysis of Distributed Electric Propulsion Tilt-Rotor UAV0
Wake Vortex Far-Field of a Generic Transport Aircraft Affected by Oscillating Flaps0
Research on Fuel-Saving and Environmentally Friendly Approach Trajectory Considering Air Traffic Management Intention0
Wind Tunnel and Grid Resolution Effects in Large-Eddy Simulations of the High-Lift Common Research Model0
Liquid Cooling Systems for Batteries of Electric Vertical Takeoff and Landing Aircraft0
Simplified Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics0
Fountain Flow Visualization in Quadrotor Wake Decreasing Rotor Thrust In-Ground Effect0
Numerical Evaluation on Large Ground-Effect Seaplane at Takeoff with Power Augmented Ram0
A Study of the Wind Sensing Performance of Small Pusher and Puller Hexacopters0
Aerostructural Optimization and Comparative Study of Twin-Fuselage and Strut-Braced-Wing Aircraft Configurations0
Performance Improvement of Winged Compound Helicopter Due to Differential Flap Deflections0
Experimental and Numerical Nonlinear Stability Analysis of Wings Incorporating Flared Folding Wingtips0
Structural and Aerodynamic Preliminary Design Optimization for Highly Flexible Wing–Tail Configuration0
Aerodynamic Performance of Propeller–Wing in Continuous Transition Mode Under Different Strategies0
Airfoil Morphed Leading-Edge Design for High-Lift Applications Using Genetic Algorithm0
Aircraft Simulations Using the New CFD Software from ONERA, DLR, and Airbus0
Understanding High-Speed Aeroelastic Stability of a Gimballed Proprotor0
Exploration of the Effects of Rotor Blade Twist on Whirl-Flutter Stability Boundaries0
Wall-Modeled Large-Eddy Simulation Method for Unstructured-Grid Navier–Stokes Solvers0
HLPW-4/GMGW-3: High-Order Discretization Technology Focus Group Workshop Summary0
Assessment of an Open-Source Aircraft Noise Prediction Model Using Approach Phase Measurements0
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design0
Sprayed Liquid Flaps: A Numerical Assessment of a Multiphase Jet Concept0
Retrospective and Recent Examples of Aircraft and Rotorcraft System Identification at DLR0
Preliminary Design Criteria for Supersonic Biplane0
Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics0
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