AIAA Journal

Papers
(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 2020-04-01 to 2024-04-01.)
ArticleCitations
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines91
Efficient Aerodynamic Shape Optimization with Deep-Learning-Based Geometric Filtering87
Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization74
Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks66
Learning Physics-Based Reduced-Order Models for a Single-Injector Combustion Process62
Hypersonic Fluid–Structure Interactions in Compression Corner Shock-Wave/Boundary-Layer Interaction54
Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach48
Analysis of the Detonation Wave Structure in a Linearized Rotating Detonation Engine46
Numerical Study on JP-10/Air Detonation and Rotating Detonation Engine45
High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design44
Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators44
Supersonic and Hypersonic Drag Coefficients for a Sphere41
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions40
Improvements to the Quadratic Constitutive Relation Based on NASA Juncture Flow Data37
Data-Driven Aerospace Engineering: Reframing the Industry with Machine Learning37
Quad-Rotor Flight Simulation in Realistic Atmospheric Conditions36
Propulsion Performance of Cylindrical Rotating Detonation Engine33
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators32
Lift Regulation During Transverse Gust Encounters Using a Modified Goman–Khrabrov Model32
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning31
Self-Deployable, Self-Stiffening, and Retractable Origami-Based Arrays for Spacecraft31
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data31
Sound Propagation of Three-Dimensional Sandwich Panels: Influence of Three-Dimensional Re-Entrant Auxetic Core30
Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section30
Correction to the Spalart–Allmaras Turbulence Model, Providing More Accurate Skin Friction30
Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers30
A Benchmark Study of Kinetic Models for Shock Waves29
Experimental Aeroelastic Benchmark of a Very Flexible Wing28
Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil28
Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer27
Double–Double: New Family of Composite Laminates26
Deep Learning Based Reduced Order Model for Airfoil-Gust and Aeroelastic Interaction26
Focused Laser Differential Interferometry with Contoured Tunnel Windows26
Data-Driven Forecasting of Postflutter Responses of Geometrically Nonlinear Wings26
Verification of Anisotropic Mesh Adaptation for Turbulent Simulations over ONERA M6 Wing26
Modal Rotations: A Modal-Based Method for Large Structural Deformations of Slender Bodies26
Effect of Transverse Gust Velocity Profiles26
Shock-Wave/Boundary-Layer Interactions at Compression Ramps Studied by High-Speed Schlieren25
Ritz Solution for Transient Analysis of Variable-Stiffness Shell Structures25
Fully Local Transition Closure Model for Hypersonic Boundary Layers Considering Crossflow Effects25
Vortices Induced by a Dielectric Barrier Discharge Plasma Actuator Under Burst-Mode Actuation25
Cumulative Damage Modeling with Recurrent Neural Networks25
Measurements of Reflected Shock Tunnel Freestream Nitric Oxide Temperatures and Partial Pressure25
Thrust and Acoustic Performance of Small-Scale, Coaxial, Corotating Rotors in Hover24
Aerodynamic Data Fusion Toward the Digital Twin Paradigm24
Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination23
Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling23
General Drag Coefficient for Flow over Spherical Particles23
Single-Pixel Particle Image Velocimetry for Characterization of Dielectric Barrier Discharge Plasma Actuators23
Performance of Wall-Modeled LES with Boundary-Layer-Conforming Grids for External Aerodynamics22
Unsteady Flow Features Across Different Shock/Boundary-Layer Interaction Configurations22
Theoretical and Numerical Investigation on Total Pressure Gain in Rotating Detonation Engine22
Assessment of Low-Dissipative Shock-Capturing Schemes for the Compressible Taylor–Green Vortex22
Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions22
Smart Solar Array Consisting of Shape-Memory Releasing Mechanisms and Deployable Hinges22
Influence of Turbulence on Cambered and Symmetrical Airfoils at Low Reynolds Numbers22
Novel Numerical Approach for Free Vibration of Nanocomposite Joined Conical–Cylindrical–Conical Shells21
Control of Pressure Oscillations Induced by Supersonic Cavity Flow21
Thermal Nonlinear Buckling of Shear Deformable Functionally Graded Cylindrical Shells with Porosities21
Experiments on High-Temperature Hypersonic Fluid–Structure Interaction with Plastic Deformation21
Compressible Velocity Transformations for Various Noncanonical Wall-Bounded Turbulent Flows21
Surface Step Effects on Boundary-Layer Transition Dominated by Tollmien–Schlichting Instability20
Equivalent Dynamic Model of the Space Antenna Truss with Initial Stress20
High-Fidelity Simulations of Noise Generation in a Propeller-Driven Unmanned Aerial Vehicle20
Adjoint-Free Aerodynamic Shape Optimization of the Common Research Model Wing20
Overview of the Use of Large-Eddy Simulations in Jet Aeroacoustics20
Parametric Experimental Studies on Supersonic Flow Unsteadiness over a Hemispherical Spiked Body20
Time-Accurate Experimental Investigation of Hypersonic Inlet Buzz at Mach 519
Effects of Fluidic Oscillator Nozzle Angle on the Flowfield and Impingement Heat Transfer19
Wavelet-Based Adaptive Unsteady Reynolds-Averaged Navier–Stokes Simulations of Wall-Bounded Compressible Turbulent Flows19
Controlling Flow Separation on a Thick Airfoil Using Backward Traveling Waves19
Gaussian Process Surrogate Model with Composite Kernel Learning for Engineering Design19
Real-Time Prediction of Probabilistic Crack Growth with a Helicopter Component Digital Twin19
Influence of Leading-Edge Tubercle with Amplitude Modulation on NACA 0015 Airfoil19
Numerical Method for Particulate-Induced High-Speed Boundary-Layer Transition Simulations19
Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment19
Fast Predictions of Aircraft Aerodynamics Using Deep-Learning Techniques18
Investigation of Blowing and Suction for Turbulent Flow Control on Airfoils18
Shock-Induced Flow Separation in an Overexpanded Supersonic Planar Nozzle18
Estimation of Inflow Uncertainties in Laminar Hypersonic Double-Cone Experiments18
Flutter Tests of the Pazy Wing18
Analysis of Novel Morphing Trailing Edge Flap Actuated by Multistable Laminates18
Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control18
Experimental Investigation of Transverse and Vortex Gust Encounters at Low Reynolds Numbers18
Simulations of Unsteady Three-Dimensional Hypersonic Double-Wedge Flow Experiments18
Direct Simulation of Fluid–Structure Interaction in a Hypersonic Compression-Ramp Flow18
Stress States in Highly Flexible Thin-Walled Composite Structures by Unified Shell Model17
Quasi-Steady In-Ground-Effect Model for Single and Multirotor Aerial Vehicles17
Three-Dimensional Flowfield in a Fin-Generated Shock Wave/Boundary-Layer Interaction Using Tomographic PIV17
Large-Scale Forcing of a Turbulent Channel Flow Through Spanwise Synthetic Jets17
Length-Scale Correction for Reynolds-Stress Modeling17
Experimental Scramjet Combustion Modes of Hydrocarbon Mixtures at Mach 8 Flight Conditions17
Electromechanical Resonant Ice Protection Systems: Energetic and Power Considerations17
Control of Reflected Waves with Acoustic Metasurfaces for Hypersonic Boundary-Layer Stabilization17
Verification of Unstructured Grid Adaptation Components17
Physics-Informed Artificial Neural Network Approach for Axial Compression Buckling Analysis of Thin-Walled Cylinder17
Aerodynamic Prediction of Iced Airfoils Based on Modified Three-Equation Turbulence Model17
Impact of Site-Specific Thermal Residual Stress on the Fatigue of Wind-Turbine Blades17
Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps17
Vibration and Snapthrough of Fluid-Conveying Graphene-Reinforced Composite Pipes Under Low-Velocity Impact17
Modal Analysis of Acoustic Directivity in Turbulent Jets17
Machine Learning Reinforced Crystal Plasticity Modeling Under Experimental Uncertainty17
Lighthill Stress Flux Model for Ffowcs Williams–Hawkings Integrals in Frequency Domain17
Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow17
Subgrid Models, Reaction Mechanisms, and Combustion Models in Large-Eddy Simulation of Supersonic Combustion17
Cross Validation of Aerodynamic Shape Optimization Methodologies for Aircraft Wing-Body Optimization17
Pitch–Heave Symmetric Stall Flutter of a NACA0012 at Transitional Reynolds Numbers17
Vibration-Based Delamination Detection in Composite Structures Employing Mixed Unified Particle Swarm Optimization16
Simultaneous Layout and Topology Optimization of Curved Stiffened Panels16
Local Correlation-Based Transition Model for High-Speed Flows16
Self-Consistent Computational Fluid Dynamics of Supersonic Drag Reduction via Upstream-Focused Laser-Energy Deposition16
Full-Aircraft Energy-Based Force Decomposition Applied to Boundary-Layer Ingestion16
Entropy-Adjoint p-Adaptive Discontinuous Galerkin Method for the Under-Resolved Simulation of Turbulent Flows16
Nonlinear Vibration Analysis of Multidirectional Porous Functionally Graded Panel Under Thermal Environment16
Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap16
Active Manifold and Model-Order Reduction to Accelerate Multidisciplinary Analysis and Optimization16
Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition16
Permeable Leading Edges for Airfoil and Fan Noise Reduction in Disturbed Inflow16
Characterization of Laminar Separation Bubbles Using Infrared Thermography16
Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors16
Numerical Nonlinear Static Analysis of Cutout-Borne Multilayered Structures and Experimental Validation16
Flow and Noise Predictions of Coaxial Jets16
Vibration and Uncertainty Analysis of Functionally Graded Sandwich Plate Using Layerwise Theory16
Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor16
Toward a Practical Method for Hypersonic Transition Prediction Based on Stability Correlations16
Aerodynamic Characteristics of Low-Fineness-Ratio Freestream-Aligned Cylinders with Magnetic Suspension and Balance System16
Model Reduction for Steady Hypersonic Aerodynamics via Conservative Manifold Least-Squares Petrov–Galerkin Projection16
Nonlinear Aeroelastic Analysis of Highly Flexible Wings Using the Modal Rotation Method16
Laminar Separation Bubble Noise on a Propeller Operating at Low Reynolds Numbers15
Vortex Shedding Noise from Finite, Wall-Mounted, Circular Cylinders Modified with Porous Material15
Bi-Objective Adaptive Kriging for Reliability Analysis with Random and Evidence Variables15
Effect of Gust Width on Flat-Plate Response in Large Transverse Gust15
Reynolds-Averaged Numerical Simulations of Conical Shock-Wave/Boundary-Layer Interactions15
Hypersonic Oscillating Shock-Wave/Boundary-Layer Interaction on a Flat Plate15
Aeroelastic Control and Estimation with a Minimal Nonlinear Modal Description15
Nonlinear Theoretical Aeroelastic Model of a Plate: Free to Fixed In-Plane Boundaries15
Optimal Shape Adjustment of Large High-Precision Cable Network Structures15
Large-Eddy-Simulation Prediction of an Installed Jet Flow and Noise with Experimental Validation15
Generation of Excess Noise by Jets with Highly Disturbed Laminar Boundary-Layer Profiles15
Predicting Boundary-Layer Transition over Backward-Facing Steps via Linear Stability Analysis15
Gradient-Limiting Shape Control for Efficient Aerodynamic Optimization15
Wave Mode Dynamics in an Ethylene-Air Rotating Detonation Combustor15
Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics Including Convection Effects15
Lift Enhancement of a Stationary Wing in a Wake15
Smooth Local Correlation-Based Transition Model for the Spalart–Allmaras Turbulence Model15
Hybrid State Estimation for Aircraft Engine Anomaly Detection and Fault Accommodation15
Receptivity of a Hypersonic Blunt Cone: Role of Disturbances in Entropy Layer15
High-Fidelity Simulation of Turbulent Flow Past Gaussian Bump15
Aerodynamic Behavior of a Floating Offshore Wind Turbine15
Predicting Wind Turbine Wake Breakdown Using a Free Vortex Wake Code15
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints15
Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor14
Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration14
Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters14
Parametric Reduced-Order Modeling of the Unsteady Vortex-Lattice Method14
Influence of the Ground, Ceiling, and Sidewall on Micro-Quadrotors14
Large-Eddy Simulations of the Unsteady Behavior of a Hypersonic Intake at Mach 514
Background-Oriented Schlieren Imaging of Supersonic Aircraft in Flight14
Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence14
Propeller Performance at Large Angle of Attack Applicable to Compound Helicopters14
Wells Turbine Stall Control Using Plasma Actuators14
Dynamic Stall on Pitching Cambered Airfoil with Phase Offset Trailing Edge Flap14
Comparing Unstructured Adaptive Mesh Solutions for the High Lift Common Research Airfoil14
The Effect of Spatially and Temporally Modulated Plasma Actuation on Cylinder Wake14
Hot-Air Anti-Icing Heat Transfer and Surface Temperature Modeling14
Supersonic Freestream Density Fluctuations from Focused Laser Differential Interferometry and Pitot-Probe Measurements14
Quantum Speedup for Aeroscience and Engineering14
Natural Frequencies of a Heated Plate: Theory and Experiment14
Experimental Investigation of Over-the-Wing Propeller–Boundary-Layer Interaction14
Effects of Engine Acoustic Waves on Aerooptical Environment in Subsonic Flight14
Machine-Learning-Based Surrogate Modeling of Aerodynamic Flow Around Distributed Structures14
Structure of a Ship Airwake at Multiple Scales14
Active Vibration Control of a Large Space Antenna Structure Using Cable Actuator14
Defect Diagnosis in Solid Rocket Motors Using Sensors and Deep Learning Networks14
Updating Geometrically Nonlinear Reduced-Order Models Using Nonlinear Modes and Harmonic Balance14
Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 614
Randomized Algorithms for Non-Intrusive Parametric Reduced Order Modeling14
Large-Eddy Simulation of a Single Airfoil Tip-Leakage Flow13
Origami-Based Metasurfaces: Design and Radar Cross Section Reduction13
Blade Tip Vortex System of a Rotor with Cyclic Pitch13
Thermal Effect on the Performance of an Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator13
Broadband and Low-Frequency Acoustic Liner Investigations at NASA and ONERA13
Control of Fin Shock Induced Flow Separation Using Vortex Generators13
Massively Multipoint Aerodynamic Shape Design via Surrogate-Assisted Gradient-Based Optimization13
High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions13
Free Vibration Analysis of Sandwich Beams with Functionally-Graded-Cores by Complementary Functions Method13
New Development of Classical Actuator Disk Model for Propellers at Incidence13
Mechanism for Increased Viscous Drag over Porous Sheet Acoustic Liners13
Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry13
Single-Camera Three-Dimensional Velocity Measurement of a Fin-Generated Shock-Wave/Boundary-Layer Interaction13
Kinematics of Lagrangian Flow Separation in External Aerodynamics13
Reliability Analysis of Stiffened Aircraft Panels Using Adjusting Mean Value Method13
Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction13
Micro-Ramp Control for Shock Train Structure and Oscillation13
Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation13
Coupled Aerostructural Level Set Topology Optimization of Aircraft Wing Boxes13
Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface12
Koopman-Based Approach to Nonintrusive Reduced Order Modeling: Application to Aerodynamic Shape Optimization and Uncertainty Propagation12
Identification of Nonlinear Stiffness and Damping Parameters Using a Hybrid Approach12
Characterization of Post-shock Thermal Striations on a Cone/Flare12
Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios12
Effects of Double-Wedge Aft Angle on Hypersonic Laminar Flows12
Output-Based Adaptive Reynolds-Averaged Navier–Stokes Higher-Order Finite Element Solutions on a Multielement Airfoil12
HTPB Heat of Formation: Literature Survey, Group Additive Estimations, and Theoretical Effects12
Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts12
Coherence Analysis of the Noise from a Simulated Highly Heated Laboratory-Scale Jet12
Flowfield Analysis and Reconstruction of Ethylene–Air Continuous Rotating Detonation Wave12
Experimental Investigation into the Turbulence Flowfield of In-Flight Round Jets12
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods12
Supersonic Aerothermoelastic Experiments of Aerospace Structures12
Grid Generated Turbulence for Aeroacoustic Facility12
Improved Amplification Factor Transport Transition Model for Transonic Boundary Layers12
Momentum Coefficient Governing Discrete Jet Actuation for Separation Control12
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel12
Three-Dimensional Aerodynamic/Stealth Optimization Based on Adjoint Sensitivity Analysis for Scattering Problem12
Acoustical Holography-Based Analysis of Spatiospectral Lobes in High-Performance Aircraft Jet Noise12
Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators12
Novel Deicing Method Based on Plasma Synthetic Jet Actuator12
Flow and Frequency Characterization of the Synchronized Stacked Sweeping Jets12
Invertible Neural Networks for Airfoil Design12
Stability-Based Transition Model Using Transport Equations12
New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils12
Large-Eddy Simulation with Modeled Wall Stress for Complex Aerodynamics and Stall Prediction12
Influence of a Forward-Facing Step Surface Irregularity on Swept Wing Transition12
Effective Permeability of Carbon Composites Under Reentry Conditions12
Experimental Characterization of Supersonic Single- and Dual-Impinging Jets11
Numerical Analysis of Airfoil Trailing-Edge Noise for Straight and Serrated Edges at Incidence11
Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization11
Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines11
High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor11
Aerodynamic Interactions of Side-by-Side Rotors in Ground Proximity11
Flame Structure Characterization in a Dual-Mode Scramjet Using Hydroxyl Planar Laser-Induced Fluorescence11
Influence of Inlet Flow Parameters on Rotating Detonation11
High-Lift Performance Enhancement Using Active Flow Control11
Evolutionary Aeroelastic Design of Flying-Wing Cross Section11
Postprocessing of Direct Aeroacoustic Simulations Using Helmholtz Decomposition11
Dynamic Stall Control Model for Pitching Airfoils with Slot Blowing11
Multifidelity Method for Locating Aeroelastic Flutter Boundaries11
Using High-Frequency Pulsed Supersonic Microjets to Control Resonant High-Speed Cavity Flows11
Structural Analysis and Optimization of Wings Subjected to Dynamic Loads11
Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors11
Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow11
Three-Dimensional Measurement of the Crater Formation During Plume–Surface Interactions Using Stereo-Photogrammetry11
Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 411
Active Subspace Variation and Modeling Uncertainty in a Supersonic Flame Simulation11
Characteristics of a Supersonic Fluidic Oscillator Using Design of Experiment11
Supersonic Cavity Flow Subjected to Continuous and Transient Leading-Edge Blowing11
Engineering Model for Transition Prediction Based on a Hypersonic Quiet Wind Tunnel11
Simulations of Intracycle Angular Velocity Control for a Crossflow Turbine11
Evaluating the Risk of Local Optima in Aerodynamic Shape Optimization11
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