Journal of Aircraft

Papers
(The TQCC of Journal of Aircraft is 2. 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 2021-04-01 to 2025-04-01.)
ArticleCitations
Flow Control Devices for Aeroacoustic Noise Suppression in Cavity Flow16
Mixed H2/H∞ Control for Autonomous Quadrotor Landing via Linear Matrix Inequality Optimization14
Nonlinear Multibody Modeling of Flexible Aircraft with Flared Hinged Wingtips12
Energy-Harvesting Performance of an Aircraft Propeller12
Effect of Angle of Attack on Propeller Aeroacoustics at Positive and Negative Thrust11
Open-Source Framework for Sizing Hybrid and Electric General Aviation Aircraft10
System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data10
Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration9
Induced-Strain Actuators for Morphing of Multi-Element Airfoils9
Potential for Energy Recovery from Boundary-Layer Ingesting Actuator Disk Propulsion8
Numerical Modeling of Aircraft Fire: Postcrash Fire8
Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling8
Comparison of Overwing and Underwing Nacelle Aeropropulsion Optimization for Subsonic Transport Aircraft8
Optimization of Lift-Plus-Cruise Vertical Take-Off and Landing Aircraft with Electrified Propulsion8
Announcements and Acknowledgments7
Steady and Unsteady Hover Test of a Lift Compounding Rotorcraft7
Transonic Flutter Dips of the AGARD 445.6 Wing7
Unsteady Propeller Wake Interference on Wing in Tractor Configuration at Low-Reynolds-Number Condition7
Experimental Aerodynamic Analysis of a QuadPlane Unmanned Aircraft System7
Optimal Mission Profile for Low-Boom Supersonic Aircraft7
Eigenvalue Sensitivity Computations for Linear Stability Theory6
Credibility-Based Multidisciplinary Design Optimization of Hybrid and Fully Electric Aircraft6
2025 AIAA Journal of Aircraft Editorial6
Exploration of a Low-Speed, Flapped, Slotted, Natural-Laminar-Flow Airfoil6
Implementation of Fuel-Saving Relaxed Climb Procedure6
Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor6
An Enhanced Jig-Shape Approach to Lifting Propeller Design6
Metamodeling Approach for Wing Structural Sizing of Box-Wing Aircraft5
Impact of Phase Offset on the Flowfields Downstream of Synchronized Propellers5
Fire Reaction of Carbon Epoxy Composite Laminates at Small and Large Scales5
Machine Learning Models for Multirotor Performance Prediction5
Minimum Trim Drag for a Three-Surface Supersonic Transport Aircraft5
Ice Shape Convergence in Multistep Ice Accretion Simulations5
Effect of Partial Ground and Partial Ceiling on Propeller Performance5
Evaluation of Unmanned Aerial Vehicle Swarm Design Through Metrics of Survivability5
Improvement of Icing Simulation with Novel Ice Crystal Sticking Model5
Transonic Corrections for the Unsteady Compressible Source and Doublet Panel Method5
Plasma Gurney Flap Flight Control at Low Angle of Attack4
High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring4
Fluid–Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft4
Geometrically Nonlinear Coupled Adjoint Aerostructural Optimization of Natural-Laminar-Flow Strut-Braced Wing4
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
Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft4
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
Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft4
Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft3
Assessment of Potential Commercial Success of Business Jets with Natural Laminar Flow3
Fuel Cell Hybrid-Electric Aircraft: Design, Operational, and Environmental Impact3
Experimental Investigation of the Active Flow Control over a Cranked-Delta Wing3
Including Blade Elasticity into Frequency-Domain Propeller Whirl Flutter Analysis3
Actuator Surface Modeling of Rotors at the Ship–Helicopter Dynamic Interface3
Piezoelectric-Actuator De-Icing Array Design Based on Structural Vibration Modes3
Fleet Design Optimization of Package Delivery Unmanned Aerial Vehicles Considering Operations3
Level-Set Mass-Conservative Front-Tracking Technique for Multistep Simulations of In-Flight Ice Accretion3
Propeller Rotation Effects on Pitching Moment for Transport Aircraft with Conventional Tail3
Structural Optimization of a Large-Scale 3D-Printed High-Altitude Propeller Blade with Experimental Validation3
Solid-State Electroaerodynamic Aircraft Design Using Signomial Programming3
Modeling Aircraft Fuel Jettison Using Smoothed Particle Hydrodynamics on Finite-Volume Meshes3
Aerodynamic Stability Derivative Calculations Using the Compressible Source and Doublet Panel Method3
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles3
Uncertainty Quantification of the ONERA 7A Rotor Performance and Loads Using Comprehensive Analysis3
Design Exploration of Transonic Airfoils for Natural and Hybrid Laminar Flow Control Applications3
Experimental Investigation of the Coupling Process of Laminar Wings at Their Tips3
Predicting Transonic Buffet Onset for the Boeing Transonic Truss-Braced Wing Aircraft3
Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water3
Control Authority of a Single-Surface Parafoil with Bleed-Air Spoilers3
Influence of Stitch Angle on the Flexural Response of Composite Structures2
Application of the Ornstein–Uhlenbeck Process to Generate Stochastic Vertical Wind Profiles2
Experimental Results for a Low-Reynolds-Number Airfoil in a Low-Turbulence Wind Tunnel2
Pseudospectral-Method-Based Framework for Rotorcraft Stability and Trim Analysis2
Terrain Envelope for Landing Stability of a Multirotor UAV with Adaptive Landing Gear2
Advances and Modern Applications of Frequency-Domain Aircraft and Rotorcraft System Identification2
Comparison of Data-Driven Approaches to Rotorcraft Store Separation Modeling2
Investigation of Aerodynamic Support Interference for Testing a Semispan T Tail Aircraft Model2
Neural-Network-Based Model for Trailing-Edge Flap Loads in Preliminary Aircraft Design2
Massive Graphical Processing Unit Parallelization for Multirotor Computational Fluid Dynamics2
Scale Effects in Wind Tunnel Testing: Extrapolation of the Drag Coefficient2
Three-Dimensional Aeromechanical Analysis of Lift Offset Coaxial Rotors: A Helios Test Case2
Zonal Safety and Particular Risk Analysis for Early Aircraft Design2
Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing2
Experimental Investigation and Numerical Modeling of Noise Generated by Installed Pusher Propellers2
Conceptual Design of Aircraft System Routing Architectures Using a Bio-Inspired Algorithm2
Macro- and Mesoscopic Design for Cabin Door Pretightened Fabric Rubber Seal Structure2
Certification-Constrained Vertical Tail Sizing and Power Split Optimization for Distributed Electric Propulsion Aircraft2
Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations2
Propulsion–Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport2
Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation2
Steady Solutions for Supersonic Transport Takeoffs with a Variable Noise Reduction System2
Numerical Investigation of an Unmanned Aerial Vehicle Launch from Military Transport Aircrafts2
Line-Based High-Order Hybrid Scheme on Unstructured Grids for Compressible Flows2
Unsteady Effects of Blowing over Actuated Surfaces Using Phase-Locked Particle Image Velocimetry2
Holistic Approach for Aircraft Trajectory Optimization Using Optimal Control2
Introduction to the Advances in Aircraft System Identification from Flight Test Data Virtual Collection2
Theodorsen’s and Garrick’s Flutter Calculations: Revisited2
Forecasting the Operational Lifetime of Battery-Powered Electric Aircraft2
Correlation of High-Speed Tiltrotor Stability Predictions with Test Data and Parametric Study2
Introduction to the Selected Papers from NATO AVT-338 Specialists Meeting on Advanced Wind Tunnel Boundary Simulation II Virtual Collection2
Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization2
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