AIAA Journal

(The TQCC of AIAA Journal is 6. 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 2020-07-01 to 2024-07-01.)
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines104
Efficient Aerodynamic Shape Optimization with Deep-Learning-Based Geometric Filtering96
Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization81
Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks73
Hypersonic Fluid–Structure Interactions in Compression Corner Shock-Wave/Boundary-Layer Interaction57
High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design52
Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach51
Numerical Study on JP-10/Air Detonation and Rotating Detonation Engine50
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions47
Analysis of the Detonation Wave Structure in a Linearized Rotating Detonation Engine47
Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators46
Supersonic and Hypersonic Drag Coefficients for a Sphere46
Data-Driven Aerospace Engineering: Reframing the Industry with Machine Learning45
Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers44
Improved Amplification Factor Transport Transition Model for Transonic Boundary Layers42
Improvements to the Quadratic Constitutive Relation Based on NASA Juncture Flow Data37
Propulsion Performance of Cylindrical Rotating Detonation Engine36
Sound Propagation of Three-Dimensional Sandwich Panels: Influence of Three-Dimensional Re-Entrant Auxetic Core36
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning35
Double–Double: New Family of Composite Laminates35
Lift Regulation During Transverse Gust Encounters Using a Modified Goman–Khrabrov Model34
Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section34
Self-Deployable, Self-Stiffening, and Retractable Origami-Based Arrays for Spacecraft34
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators33
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data33
Experimental Aeroelastic Benchmark of a Very Flexible Wing31
General Drag Coefficient for Flow over Spherical Particles31
Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil29
Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer28
Deep Learning Based Reduced Order Model for Airfoil-Gust and Aeroelastic Interaction28
Effect of Transverse Gust Velocity Profiles28
Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling27
Focused Laser Differential Interferometry with Contoured Tunnel Windows27
Complex Standard Eigenvalue Problem Derivative Computation for Laminar–Turbulent Transition Prediction27
Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination26
Cumulative Damage Modeling with Recurrent Neural Networks26
High-Fidelity Simulations of Noise Generation in a Propeller-Driven Unmanned Aerial Vehicle26
Measurements of Reflected Shock Tunnel Freestream Nitric Oxide Temperatures and Partial Pressure26
Fast Predictions of Aircraft Aerodynamics Using Deep-Learning Techniques26
Modal Rotations: A Modal-Based Method for Large Structural Deformations of Slender Bodies26
Smart Solar Array Consisting of Shape-Memory Releasing Mechanisms and Deployable Hinges25
Assessment of Low-Dissipative Shock-Capturing Schemes for the Compressible Taylor–Green Vortex25
Fully Local Transition Closure Model for Hypersonic Boundary Layers Considering Crossflow Effects25
Single-Pixel Particle Image Velocimetry for Characterization of Dielectric Barrier Discharge Plasma Actuators25
Compressible Velocity Transformations for Various Noncanonical Wall-Bounded Turbulent Flows25
Aerodynamic Data Fusion Toward the Digital Twin Paradigm25
Laminar Separation Bubble Noise on a Propeller Operating at Low Reynolds Numbers24
Surface Step Effects on Boundary-Layer Transition Dominated by Tollmien–Schlichting Instability23
Quasi-Steady In-Ground-Effect Model for Single and Multirotor Aerial Vehicles23
Aerodynamic Prediction of Iced Airfoils Based on Modified Three-Equation Turbulence Model23
Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions23
Theoretical and Numerical Investigation on Total Pressure Gain in Rotating Detonation Engine23
Influence of Leading-Edge Tubercle with Amplitude Modulation on NACA 0015 Airfoil22
Controlling Flow Separation on a Thick Airfoil Using Backward Traveling Waves22
Unsteady Flow Features Across Different Shock/Boundary-Layer Interaction Configurations22
Novel Numerical Approach for Free Vibration of Nanocomposite Joined Conical–Cylindrical–Conical Shells22
Thermal Nonlinear Buckling of Shear Deformable Functionally Graded Cylindrical Shells with Porosities22
Adjoint-Free Aerodynamic Shape Optimization of the Common Research Model Wing22
Electromechanical Resonant Ice Protection Systems: Energetic and Power Considerations22
Performance of Wall-Modeled LES with Boundary-Layer-Conforming Grids for External Aerodynamics22
Analysis of Novel Morphing Trailing Edge Flap Actuated by Multistable Laminates21
Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment21
Parametric Experimental Studies on Supersonic Flow Unsteadiness over a Hemispherical Spiked Body20
Experimental Investigation of Transverse and Vortex Gust Encounters at Low Reynolds Numbers20
Verification of Unstructured Grid Adaptation Components20
Flow and Noise Predictions of Coaxial Jets20
Modal Analysis of Acoustic Directivity in Turbulent Jets20
Stress States in Highly Flexible Thin-Walled Composite Structures by Unified Shell Model20
Estimation of Inflow Uncertainties in Laminar Hypersonic Double-Cone Experiments19
Investigation of Blowing and Suction for Turbulent Flow Control on Airfoils19
Impact of Site-Specific Thermal Residual Stress on the Fatigue of Wind-Turbine Blades19
Real-Time Prediction of Probabilistic Crack Growth with a Helicopter Component Digital Twin19
Aerodynamic Behavior of a Floating Offshore Wind Turbine19
Numerical Method for Particulate-Induced High-Speed Boundary-Layer Transition Simulations19
Permeable Leading Edges for Airfoil and Fan Noise Reduction in Disturbed Inflow19
Nonlinear Vibration Analysis of Multidirectional Porous Functionally Graded Panel Under Thermal Environment19
Effects of Fluidic Oscillator Nozzle Angle on the Flowfield and Impingement Heat Transfer19
Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow19
Direct Simulation of Fluid–Structure Interaction in a Hypersonic Compression-Ramp Flow19
Machine Learning Reinforced Crystal Plasticity Modeling Under Experimental Uncertainty19
Flutter Tests of the Pazy Wing18
Local Correlation-Based Transition Model for High-Speed Flows18
Model Reduction for Steady Hypersonic Aerodynamics via Conservative Manifold Least-Squares Petrov–Galerkin Projection18
Predicting Boundary-Layer Transition over Backward-Facing Steps via Linear Stability Analysis18
Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps18
Propeller Performance at Large Angle of Attack Applicable to Compound Helicopters18
Vibration and Snapthrough of Fluid-Conveying Graphene-Reinforced Composite Pipes Under Low-Velocity Impact18
Predicting Wind Turbine Wake Breakdown Using a Free Vortex Wake Code18
Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control18
Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap18
Simulations of Unsteady Three-Dimensional Hypersonic Double-Wedge Flow Experiments18
Pitch–Heave Symmetric Stall Flutter of a NACA0012 at Transitional Reynolds Numbers18
Control of Reflected Waves with Acoustic Metasurfaces for Hypersonic Boundary-Layer Stabilization18
Characterization of Laminar Separation Bubbles Using Infrared Thermography18
Experimental Scramjet Combustion Modes of Hydrocarbon Mixtures at Mach 8 Flight Conditions18
High-Fidelity Simulation of Turbulent Flow Past Gaussian Bump18
Vibration-Based Delamination Detection in Composite Structures Employing Mixed Unified Particle Swarm Optimization17
Vibration and Uncertainty Analysis of Functionally Graded Sandwich Plate Using Layerwise Theory17
Experimental Investigation of Over-the-Wing Propeller–Boundary-Layer Interaction17
Grid Generated Turbulence for Aeroacoustic Facility17
Influence of the Ground, Ceiling, and Sidewall on Micro-Quadrotors17
Smooth Local Correlation-Based Transition Model for the Spalart–Allmaras Turbulence Model17
Receptivity of a Hypersonic Blunt Cone: Role of Disturbances in Entropy Layer17
Simultaneous Layout and Topology Optimization of Curved Stiffened Panels17
Active Manifold and Model-Order Reduction to Accelerate Multidisciplinary Analysis and Optimization17
Full-Aircraft Energy-Based Force Decomposition Applied to Boundary-Layer Ingestion17
Nonlinear Aeroelastic Analysis of Highly Flexible Wings Using the Modal Rotation Method17
Subgrid Models, Reaction Mechanisms, and Combustion Models in Large-Eddy Simulation of Supersonic Combustion17
Continuous Tow Steering Around an Elliptical Cutout in a Composite Panel17
Gradient-Limiting Shape Control for Efficient Aerodynamic Optimization17
Lighthill Stress Flux Model for Ffowcs Williams–Hawkings Integrals in Frequency Domain17
Hot-Air Anti-Icing Heat Transfer and Surface Temperature Modeling17
Optimal Shape Adjustment of Large High-Precision Cable Network Structures17
Three-Dimensional Flowfield in a Fin-Generated Shock Wave/Boundary-Layer Interaction Using Tomographic PIV17
Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters16
Aerodynamic Characteristics of Low-Fineness-Ratio Freestream-Aligned Cylinders with Magnetic Suspension and Balance System16
Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors16
Generation of Excess Noise by Jets with Highly Disturbed Laminar Boundary-Layer Profiles16
Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 616
Toward a Practical Method for Hypersonic Transition Prediction Based on Stability Correlations16
Active Vibration Control of a Large Space Antenna Structure Using Cable Actuator16
Self-Consistent Computational Fluid Dynamics of Supersonic Drag Reduction via Upstream-Focused Laser-Energy Deposition16
Entropy-Adjoint p-Adaptive Discontinuous Galerkin Method for the Under-Resolved Simulation of Turbulent Flows16
Effect of Gust Width on Flat-Plate Response in Large Transverse Gust16
Reynolds-Averaged Numerical Simulations of Conical Shock-Wave/Boundary-Layer Interactions16
Hypersonic Oscillating Shock-Wave/Boundary-Layer Interaction on a Flat Plate16
The Effect of Spatially and Temporally Modulated Plasma Actuation on Cylinder Wake16
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints16
Numerical Nonlinear Static Analysis of Cutout-Borne Multilayered Structures and Experimental Validation16
Large-Eddy Simulations of the Unsteady Behavior of a Hypersonic Intake at Mach 516
Large-Eddy Simulation of a Single Airfoil Tip-Leakage Flow16
Quantum Advantage in Cryptography16
Quantum Speedup for Aeroscience and Engineering15
Dynamic Stall on Pitching Cambered Airfoil with Phase Offset Trailing Edge Flap15
Reliability Analysis of Stiffened Aircraft Panels Using Adjusting Mean Value Method15
Nonlinear Theoretical Aeroelastic Model of a Plate: Free to Fixed In-Plane Boundaries15
Influence of a Forward-Facing Step Surface Irregularity on Swept Wing Transition15
Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence15
Randomized Algorithms for Non-Intrusive Parametric Reduced Order Modeling15
Deep Learning for Multifidelity Aerodynamic Distribution Modeling from Experimental and Simulation Data15
Wave Mode Dynamics in an Ethylene-Air Rotating Detonation Combustor15
New Development of Classical Actuator Disk Model for Propellers at Incidence15
HTPB Heat of Formation: Literature Survey, Group Additive Estimations, and Theoretical Effects15
Updating Geometrically Nonlinear Reduced-Order Models Using Nonlinear Modes and Harmonic Balance15
Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor15
Machine-Learning-Based Surrogate Modeling of Aerodynamic Flow Around Distributed Structures15
Aeroelastic Control and Estimation with a Minimal Nonlinear Modal Description15
Lift Enhancement of a Stationary Wing in a Wake15
Invertible Neural Networks for Airfoil Design14
Supersonic Freestream Density Fluctuations from Focused Laser Differential Interferometry and Pitot-Probe Measurements14
Momentum Coefficient Governing Discrete Jet Actuation for Separation Control14
Background-Oriented Schlieren Imaging of Supersonic Aircraft in Flight14
Numerical Analysis of Airfoil Trailing-Edge Noise for Straight and Serrated Edges at Incidence14
Wells Turbine Stall Control Using Plasma Actuators14
Origami-Based Metasurfaces: Design and Radar Cross Section Reduction14
Defect Diagnosis in Solid Rocket Motors Using Sensors and Deep Learning Networks14
Coupled Aerostructural Level Set Topology Optimization of Aircraft Wing Boxes14
Single-Camera Three-Dimensional Velocity Measurement of a Fin-Generated Shock-Wave/Boundary-Layer Interaction14
Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration14
Supersonic Aerothermoelastic Experiments of Aerospace Structures14
Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios14
Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation14
Broadband and Low-Frequency Acoustic Liner Investigations at NASA and ONERA14
Natural Frequencies of a Heated Plate: Theory and Experiment14
Effects of Engine Acoustic Waves on Aerooptical Environment in Subsonic Flight14
Comparing Unstructured Adaptive Mesh Solutions for the High Lift Common Research Airfoil14
Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction13
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel13
Flowfield Analysis and Reconstruction of Ethylene–Air Continuous Rotating Detonation Wave13
Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry13
Postprocessing of Direct Aeroacoustic Simulations Using Helmholtz Decomposition13
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods13
Free Vibration Analysis of Sandwich Beams with Functionally-Graded-Cores by Complementary Functions Method13
New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils13
Acoustical Holography-Based Analysis of Spatiospectral Lobes in High-Performance Aircraft Jet Noise13
Coherence Analysis of the Noise from a Simulated Highly Heated Laboratory-Scale Jet13
Nonconvex L1/2 Minimization Based Compressive Sensing Approach for Duct Azimuthal Mode Detection13
Control of Fin Shock Induced Flow Separation Using Vortex Generators13
High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions13
Blade Tip Vortex System of a Rotor with Cyclic Pitch13
Thermal Effect on the Performance of an Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator13
Stability-Based Transition Model Using Transport Equations13
Micro-Ramp Control for Shock Train Structure and Oscillation13
Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface13
Mechanism for Increased Viscous Drag over Porous Sheet Acoustic Liners13
Experimental Investigation into the Turbulence Flowfield of In-Flight Round Jets13
Effective Permeability of Carbon Composites Under Reentry Conditions13
Flow and Frequency Characterization of the Synchronized Stacked Sweeping Jets13
Aerodynamic Interactions of Side-by-Side Rotors in Ground Proximity13
Surrogate Modeling Accelerated Shape Optimization of Deployable Composite Tape-Spring Hinges12
Experimental Investigation of Transonic Shock Buffet on an OAT15A Profile12
Flame Structure Characterization in a Dual-Mode Scramjet Using Hydroxyl Planar Laser-Induced Fluorescence12
Direct Numerical Simulation of Flow over a Triangular Airfoil Under Martian Conditions12
Evaluating the Risk of Local Optima in Aerodynamic Shape Optimization12
High-Lift Performance Enhancement Using Active Flow Control12
Effect of Aspect Ratio on Finite-Wing Dynamic Stall12
High-Order Resolution of Multidimensional Compressible Reactive Flow Using Implicit Shock Tracking12
Identification of Nonlinear Stiffness and Damping Parameters Using a Hybrid Approach12
Magnetohydrodynamic Drag Measurements in an Expansion Tunnel with Argon Test Gas12
Structural Analysis and Optimization of Wings Subjected to Dynamic Loads12
Simulations of Intracycle Angular Velocity Control for a Crossflow Turbine12
Flow Characterization of Porous Ultra-High-Temperature Ceramics for Transpiration Cooling12
Tones in the Acoustic Far Field of Jets in the Upstream Direction12
Low-Speed Turbofan Aerodynamic and Acoustic Prediction with an Isothermal Lattice Boltzmann Method12
Numerical Investigation of Aeroelastic Characteristics of Grid Fin12
Parabolized Stability Analysis of Hypersonic Thermal–Chemical Nonequilibrium Boundary-Layer Flows12
Novel Deicing Method Based on Plasma Synthetic Jet Actuator12
Accelerated Wind-Turbine Wake Recovery Through Actuation of the Tip-Vortex Instability12
Learning for Predictions: Real-Time Reliability Assessment of Aerospace Systems12
Output-Based Adaptive Reynolds-Averaged Navier–Stokes Higher-Order Finite Element Solutions on a Multielement Airfoil12
Large-Eddy Simulation with Modeled Wall Stress for Complex Aerodynamics and Stall Prediction12
Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts12
Transfer Learning for Flow Reconstruction Based on Multifidelity Data12
Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines12
Unsteady Aeroelastic Analysis of the Semi Aeroelastic Hinge Including Local Geometric Nonlinearities12
Supersonic Cavity Flow Subjected to Continuous and Transient Leading-Edge Blowing11
A Database for Reduced-Complexity Modeling of Fluid Flows11
Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors11
Unsteady Aerodynamic Response of a Flat Plate Encountering Large-Amplitude Sharp-Edged Gust11
Flutter Optimization of a Wing–Engine System with Passive and Active Control Approaches11
Internal Geometry Effects on Inherent Damping Performance of Additively Manufactured Components11
Parametric Uncertainty Analysis for Impedance Eduction Based on Prony’s Method11
Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 411
Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow11
Improved Nonlinear Analysis of a Propeller Blade Based on Hyper-Reduction11
Large-Eddy Simulations of Idealized Shock/Boundary-Layer Interactions with Crossflow11
Dynamic Stall Control Model for Pitching Airfoils with Slot Blowing11
Aeroacoustics of Twin Rectangular Jets Including Screech: Large-Eddy Simulations with Experimental Validation11
Fast Fourier Transformation Computation of Modal Transfer Function for Rotating Source Localization11
Effects of Reynolds Number on Swept Shock-Wave/Boundary-Layer Interactions11
Spray Characteristics of Standard and Alternative Aviation Fuels at Cold-start Conditions11
Engineering Model for Transition Prediction Based on a Hypersonic Quiet Wind Tunnel11
Three-Dimensional Measurement of the Crater Formation During Plume–Surface Interactions Using Stereo-Photogrammetry11
Investigation of the Low-Frequency Oscillations in the Flowfield About an Airfoil11
Evolutionary Aeroelastic Design of Flying-Wing Cross Section11
Efficient Bilevel Surrogate Approach for Optimization Under Uncertainty of Shock Control Bumps11
Analytical Method of Evaluating Nonuniformities in Shock Tube Flows: Theory and Development11
High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor11
Using High-Frequency Pulsed Supersonic Microjets to Control Resonant High-Speed Cavity Flows11
Application of Leading-Edge Tubercles to Enhance Propeller Performance11
Flux Reconstruction Implementation of an Algebraic Wall Model for Large-Eddy Simulation11
Numerical Investigation of Sweep Effect on Turbulent Shock-Wave Boundary-Layer Interaction11
Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models11
Influence of Inlet Flow Parameters on Rotating Detonation11
Bayesian Support Vector Regression for Reliability-Based Design Optimization11
Proper Orthogonal Decomposition of High-Speed Particle Image Velocimetry in an Open Cavity11
Experimental Characterization of Supersonic Single- and Dual-Impinging Jets11
Numerical Investigation of Nonlinear Boundary-Layer Transition for Cones at Mach 611
Active Subspace Variation and Modeling Uncertainty in a Supersonic Flame Simulation11
Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization11