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 2020-05-01 to 2024-05-01.)
ArticleCitations
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines96
Efficient Aerodynamic Shape Optimization with Deep-Learning-Based Geometric Filtering91
Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization77
Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks69
Learning Physics-Based Reduced-Order Models for a Single-Injector Combustion Process65
Hypersonic Fluid–Structure Interactions in Compression Corner Shock-Wave/Boundary-Layer Interaction55
Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach50
High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design48
Numerical Study on JP-10/Air Detonation and Rotating Detonation Engine47
Analysis of the Detonation Wave Structure in a Linearized Rotating Detonation Engine46
Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators44
Supersonic and Hypersonic Drag Coefficients for a Sphere43
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions41
Data-Driven Aerospace Engineering: Reframing the Industry with Machine Learning38
Quad-Rotor Flight Simulation in Realistic Atmospheric Conditions37
Improvements to the Quadratic Constitutive Relation Based on NASA Juncture Flow Data37
Propulsion Performance of Cylindrical Rotating Detonation Engine34
Lift Regulation During Transverse Gust Encounters Using a Modified Goman–Khrabrov Model33
Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section33
Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers33
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data32
Sound Propagation of Three-Dimensional Sandwich Panels: Influence of Three-Dimensional Re-Entrant Auxetic Core32
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators32
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning32
Self-Deployable, Self-Stiffening, and Retractable Origami-Based Arrays for Spacecraft31
Correction to the Spalart–Allmaras Turbulence Model, Providing More Accurate Skin Friction31
Double–Double: New Family of Composite Laminates29
Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil29
A Benchmark Study of Kinetic Models for Shock Waves29
Experimental Aeroelastic Benchmark of a Very Flexible Wing28
Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer27
Focused Laser Differential Interferometry with Contoured Tunnel Windows27
Deep Learning Based Reduced Order Model for Airfoil-Gust and Aeroelastic Interaction27
Effect of Transverse Gust Velocity Profiles27
Data-Driven Forecasting of Postflutter Responses of Geometrically Nonlinear Wings26
Modal Rotations: A Modal-Based Method for Large Structural Deformations of Slender Bodies26
General Drag Coefficient for Flow over Spherical Particles25
Measurements of Reflected Shock Tunnel Freestream Nitric Oxide Temperatures and Partial Pressure25
Cumulative Damage Modeling with Recurrent Neural Networks25
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
Single-Pixel Particle Image Velocimetry for Characterization of Dielectric Barrier Discharge Plasma Actuators24
Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination24
Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling24
Aerodynamic Data Fusion Toward the Digital Twin Paradigm24
Influence of Turbulence on Cambered and Symmetrical Airfoils at Low Reynolds Numbers23
Assessment of Low-Dissipative Shock-Capturing Schemes for the Compressible Taylor–Green Vortex23
Compressible Velocity Transformations for Various Noncanonical Wall-Bounded Turbulent Flows22
Theoretical and Numerical Investigation on Total Pressure Gain in Rotating Detonation Engine22
Surface Step Effects on Boundary-Layer Transition Dominated by Tollmien–Schlichting Instability22
Performance of Wall-Modeled LES with Boundary-Layer-Conforming Grids for External Aerodynamics22
Unsteady Flow Features Across Different Shock/Boundary-Layer Interaction Configurations22
Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions22
Smart Solar Array Consisting of Shape-Memory Releasing Mechanisms and Deployable Hinges22
Controlling Flow Separation on a Thick Airfoil Using Backward Traveling Waves21
Adjoint-Free Aerodynamic Shape Optimization of the Common Research Model Wing21
Thermal Nonlinear Buckling of Shear Deformable Functionally Graded Cylindrical Shells with Porosities21
Novel Numerical Approach for Free Vibration of Nanocomposite Joined Conical–Cylindrical–Conical Shells21
Control of Pressure Oscillations Induced by Supersonic Cavity Flow21
Parametric Experimental Studies on Supersonic Flow Unsteadiness over a Hemispherical Spiked Body20
Time-Accurate Experimental Investigation of Hypersonic Inlet Buzz at Mach 520
Scale-Resolving Simulations of a Civil Aircraft Wing Transonic Shock-Buffet Experiment20
High-Fidelity Simulations of Noise Generation in a Propeller-Driven Unmanned Aerial Vehicle20
Analysis of Novel Morphing Trailing Edge Flap Actuated by Multistable Laminates20
Fast Predictions of Aircraft Aerodynamics Using Deep-Learning Techniques19
Numerical Method for Particulate-Induced High-Speed Boundary-Layer Transition Simulations19
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
Effects of Fluidic Oscillator Nozzle Angle on the Flowfield and Impingement Heat Transfer19
Machine Learning Reinforced Crystal Plasticity Modeling Under Experimental Uncertainty19
Experimental Investigation of Transverse and Vortex Gust Encounters at Low Reynolds Numbers19
Electromechanical Resonant Ice Protection Systems: Energetic and Power Considerations19
Aerodynamic Prediction of Iced Airfoils Based on Modified Three-Equation Turbulence Model19
Simulations of Unsteady Three-Dimensional Hypersonic Double-Wedge Flow Experiments18
Stress States in Highly Flexible Thin-Walled Composite Structures by Unified Shell Model18
Quasi-Steady In-Ground-Effect Model for Single and Multirotor Aerial Vehicles18
Shock-Induced Flow Separation in an Overexpanded Supersonic Planar Nozzle18
Flutter Tests of the Pazy Wing18
Vibration and Snapthrough of Fluid-Conveying Graphene-Reinforced Composite Pipes Under Low-Velocity Impact18
Physics-Informed Artificial Neural Network Approach for Axial Compression Buckling Analysis of Thin-Walled Cylinder18
Large-Scale Forcing of a Turbulent Channel Flow Through Spanwise Synthetic Jets18
Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control18
Estimation of Inflow Uncertainties in Laminar Hypersonic Double-Cone Experiments18
Investigation of Blowing and Suction for Turbulent Flow Control on Airfoils18
Local Correlation-Based Transition Model for High-Speed Flows18
Direct Simulation of Fluid–Structure Interaction in a Hypersonic Compression-Ramp Flow18
Verification of Unstructured Grid Adaptation Components17
Modal Analysis of Acoustic Directivity in Turbulent Jets17
Three-Dimensional Flowfield in a Fin-Generated Shock Wave/Boundary-Layer Interaction Using Tomographic PIV17
Full-Aircraft Energy-Based Force Decomposition Applied to Boundary-Layer Ingestion17
Characterization of Laminar Separation Bubbles Using Infrared Thermography17
Subgrid Models, Reaction Mechanisms, and Combustion Models in Large-Eddy Simulation of Supersonic Combustion17
Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap17
Gradient-Limiting Shape Control for Efficient Aerodynamic Optimization17
Pitch–Heave Symmetric Stall Flutter of a NACA0012 at Transitional Reynolds Numbers17
Lighthill Stress Flux Model for Ffowcs Williams–Hawkings Integrals in Frequency Domain17
Permeable Leading Edges for Airfoil and Fan Noise Reduction in Disturbed Inflow17
Model Reduction for Steady Hypersonic Aerodynamics via Conservative Manifold Least-Squares Petrov–Galerkin Projection17
Cross Validation of Aerodynamic Shape Optimization Methodologies for Aircraft Wing-Body Optimization17
Control of Reflected Waves with Acoustic Metasurfaces for Hypersonic Boundary-Layer Stabilization17
Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor17
Nonlinear Vibration Analysis of Multidirectional Porous Functionally Graded Panel Under Thermal Environment17
Impact of Site-Specific Thermal Residual Stress on the Fatigue of Wind-Turbine Blades17
Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow17
Experimental Scramjet Combustion Modes of Hydrocarbon Mixtures at Mach 8 Flight Conditions17
Vibration-Based Delamination Detection in Composite Structures Employing Mixed Unified Particle Swarm Optimization17
Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps17
Flow and Noise Predictions of Coaxial Jets16
Reynolds-Averaged Numerical Simulations of Conical Shock-Wave/Boundary-Layer Interactions16
Toward a Practical Method for Hypersonic Transition Prediction Based on Stability Correlations16
The Effect of Spatially and Temporally Modulated Plasma Actuation on Cylinder Wake16
Entropy-Adjoint p-Adaptive Discontinuous Galerkin Method for the Under-Resolved Simulation of Turbulent Flows16
Vortex Shedding Noise from Finite, Wall-Mounted, Circular Cylinders Modified with Porous Material16
High-Fidelity Simulation of Turbulent Flow Past Gaussian Bump16
Vibration and Uncertainty Analysis of Functionally Graded Sandwich Plate Using Layerwise Theory16
Active Manifold and Model-Order Reduction to Accelerate Multidisciplinary Analysis and Optimization16
Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition16
Self-Consistent Computational Fluid Dynamics of Supersonic Drag Reduction via Upstream-Focused Laser-Energy Deposition16
Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors16
Numerical Nonlinear Static Analysis of Cutout-Borne Multilayered Structures and Experimental Validation16
Predicting Boundary-Layer Transition over Backward-Facing Steps via Linear Stability Analysis16
Simultaneous Layout and Topology Optimization of Curved Stiffened Panels16
Hypersonic Oscillating Shock-Wave/Boundary-Layer Interaction on a Flat Plate16
Aerodynamic Characteristics of Low-Fineness-Ratio Freestream-Aligned Cylinders with Magnetic Suspension and Balance System16
Laminar Separation Bubble Noise on a Propeller Operating at Low Reynolds Numbers16
Nonlinear Aeroelastic Analysis of Highly Flexible Wings Using the Modal Rotation Method16
Predicting Wind Turbine Wake Breakdown Using a Free Vortex Wake Code15
Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints15
Large-Eddy-Simulation Prediction of an Installed Jet Flow and Noise with Experimental Validation15
Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 615
Updating Geometrically Nonlinear Reduced-Order Models Using Nonlinear Modes and Harmonic Balance15
Effect of Gust Width on Flat-Plate Response in Large Transverse Gust15
Aerodynamic Behavior of a Floating Offshore Wind Turbine15
Parametric Reduced-Order Modeling of the Unsteady Vortex-Lattice Method15
Lift Enhancement of a Stationary Wing in a Wake15
Optimal Shape Adjustment of Large High-Precision Cable Network Structures15
Large-Eddy Simulations of the Unsteady Behavior of a Hypersonic Intake at Mach 515
Receptivity of a Hypersonic Blunt Cone: Role of Disturbances in Entropy Layer15
Dynamic Stall on Pitching Cambered Airfoil with Phase Offset Trailing Edge Flap15
Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters15
Aeroelastic Control and Estimation with a Minimal Nonlinear Modal Description15
Nonlinear Theoretical Aeroelastic Model of a Plate: Free to Fixed In-Plane Boundaries15
Smooth Local Correlation-Based Transition Model for the Spalart–Allmaras Turbulence Model15
Quantum Speedup for Aeroscience and Engineering15
Generation of Excess Noise by Jets with Highly Disturbed Laminar Boundary-Layer Profiles15
Machine-Learning-Based Surrogate Modeling of Aerodynamic Flow Around Distributed Structures15
Wave Mode Dynamics in an Ethylene-Air Rotating Detonation Combustor15
Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor14
Wells Turbine Stall Control Using Plasma Actuators14
Origami-Based Metasurfaces: Design and Radar Cross Section Reduction14
Active Vibration Control of a Large Space Antenna Structure Using Cable Actuator14
Defect Diagnosis in Solid Rocket Motors Using Sensors and Deep Learning Networks14
Momentum Coefficient Governing Discrete Jet Actuation for Separation Control14
Background-Oriented Schlieren Imaging of Supersonic Aircraft in Flight14
Randomized Algorithms for Non-Intrusive Parametric Reduced Order Modeling14
Propeller Performance at Large Angle of Attack Applicable to Compound Helicopters14
Experimental Investigation of Over-the-Wing Propeller–Boundary-Layer Interaction14
Comparing Unstructured Adaptive Mesh Solutions for the High Lift Common Research Airfoil14
New Development of Classical Actuator Disk Model for Propellers at Incidence14
Improved Amplification Factor Transport Transition Model for Transonic Boundary Layers14
Supersonic Freestream Density Fluctuations from Focused Laser Differential Interferometry and Pitot-Probe Measurements14
Natural Frequencies of a Heated Plate: Theory and Experiment14
Effects of Engine Acoustic Waves on Aerooptical Environment in Subsonic Flight14
Continuous Tow Steering Around an Elliptical Cutout in a Composite Panel14
Wall-Pressure Fluctuations Induced by a Compressible Jet in Installed Configuration14
Structure of a Ship Airwake at Multiple Scales14
Hot-Air Anti-Icing Heat Transfer and Surface Temperature Modeling14
Influence of the Ground, Ceiling, and Sidewall on Micro-Quadrotors14
HTPB Heat of Formation: Literature Survey, Group Additive Estimations, and Theoretical Effects14
Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence14
Coherence Analysis of the Noise from a Simulated Highly Heated Laboratory-Scale Jet13
Large-Eddy Simulation of a Single Airfoil Tip-Leakage Flow13
Experimental Investigation into the Turbulence Flowfield of In-Flight Round Jets13
Flow and Frequency Characterization of the Synchronized Stacked Sweeping Jets13
Mechanism for Increased Viscous Drag over Porous Sheet Acoustic Liners13
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods13
Control of Fin Shock Induced Flow Separation Using Vortex Generators13
Stability-Based Transition Model Using Transport Equations13
Thermal Effect on the Performance of an Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator13
Influence of a Forward-Facing Step Surface Irregularity on Swept Wing Transition13
Single-Camera Three-Dimensional Velocity Measurement of a Fin-Generated Shock-Wave/Boundary-Layer Interaction13
Massively Multipoint Aerodynamic Shape Design via Surrogate-Assisted Gradient-Based Optimization13
Characterization of Post-shock Thermal Striations on a Cone/Flare13
Reliability Analysis of Stiffened Aircraft Panels Using Adjusting Mean Value Method13
Three-Dimensional Aerodynamic/Stealth Optimization Based on Adjoint Sensitivity Analysis for Scattering Problem13
Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios13
Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry13
Grid Generated Turbulence for Aeroacoustic Facility13
Micro-Ramp Control for Shock Train Structure and Oscillation13
Broadband and Low-Frequency Acoustic Liner Investigations at NASA and ONERA13
Acoustical Holography-Based Analysis of Spatiospectral Lobes in High-Performance Aircraft Jet Noise13
Kinematics of Lagrangian Flow Separation in External Aerodynamics13
Blade Tip Vortex System of a Rotor with Cyclic Pitch13
High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions13
Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation13
Free Vibration Analysis of Sandwich Beams with Functionally-Graded-Cores by Complementary Functions Method13
Coupled Aerostructural Level Set Topology Optimization of Aircraft Wing Boxes13
Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction13
Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines12
Invertible Neural Networks for Airfoil Design12
Simulations of Intracycle Angular Velocity Control for a Crossflow Turbine12
High-Lift Performance Enhancement Using Active Flow Control12
Large-Eddy Simulation with Modeled Wall Stress for Complex Aerodynamics and Stall Prediction12
Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface12
Postprocessing of Direct Aeroacoustic Simulations Using Helmholtz Decomposition12
Quantum Advantage in Cryptography12
High-Order Resolution of Multidimensional Compressible Reactive Flow Using Implicit Shock Tracking12
Supersonic Aerothermoelastic Experiments of Aerospace Structures12
Output-Based Adaptive Reynolds-Averaged Navier–Stokes Higher-Order Finite Element Solutions on a Multielement Airfoil12
Evaluating the Risk of Local Optima in Aerodynamic Shape Optimization12
Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts12
Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators12
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
Novel Deicing Method Based on Plasma Synthetic Jet Actuator12
Structural Analysis and Optimization of Wings Subjected to Dynamic Loads12
New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils12
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Mach Six Quiet Tunnel12
Effective Permeability of Carbon Composites Under Reentry Conditions12
Flowfield Analysis and Reconstruction of Ethylene–Air Continuous Rotating Detonation Wave12
Nonconvex L1/2 Minimization Based Compressive Sensing Approach for Duct Azimuthal Mode Detection12
Characteristics of a Supersonic Fluidic Oscillator Using Design of Experiment12
Numerical Analysis of Airfoil Trailing-Edge Noise for Straight and Serrated Edges at Incidence11
Dynamic Stall Control Model for Pitching Airfoils with Slot Blowing11
Using High-Frequency Pulsed Supersonic Microjets to Control Resonant High-Speed Cavity Flows11
Aerodynamic Interactions of Side-by-Side Rotors in Ground Proximity11
Learning for Predictions: Real-Time Reliability Assessment of Aerospace Systems11
Influence of Inlet Flow Parameters on Rotating Detonation11
Experimental Characterization of Supersonic Single- and Dual-Impinging Jets11
Simulations of Ash and Sand Impact on a Hypersonic Forebody11
Proper Orthogonal Decomposition of High-Speed Particle Image Velocimetry in an Open Cavity11
Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 411
High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor11
Supersonic Cavity Flow Subjected to Continuous and Transient Leading-Edge Blowing11
Flame Structure Characterization in a Dual-Mode Scramjet Using Hydroxyl Planar Laser-Induced Fluorescence11
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
Internal Geometry Effects on Inherent Damping Performance of Additively Manufactured Components11
Numerical Investigation of the Unsteady Flow Past an Iced Multi-Element Airfoil11
Efficient Bilevel Surrogate Approach for Optimization Under Uncertainty of Shock Control Bumps11
Deep Learning for Multifidelity Aerodynamic Distribution Modeling from Experimental and Simulation Data11
Active Subspace Variation and Modeling Uncertainty in a Supersonic Flame Simulation11
Numerical Investigation of Aeroelastic Characteristics of Grid Fin11
Controllability Gramian as Control Design Objective in Aircraft Structural Design Optimization11
Complex Standard Eigenvalue Problem Derivative Computation for Laminar–Turbulent Transition Prediction11
Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors11
Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow11
Evolutionary Aeroelastic Design of Flying-Wing Cross Section11
Discrete Adjoint Optimization of a Hypersonic Inlet11
Numerical Investigation of Nonlinear Boundary-Layer Transition for Cones at Mach 611
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