AIAA Journal

Papers
(The median citation count of AIAA Journal 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 2021-06-01 to 2025-06-01.)
ArticleCitations
Equivalent Area Targets for Inverse Design Optimization with Changing Low-Boom Cruise Conditions87
Compounding Transient Airfoil Motions and the Effectiveness of Linear Superposition71
Numerical Nonlinear Static Analysis of Cutout-Borne Multilayered Structures and Experimental Validation70
Nonlinear Buckling and Postbuckling Analysis of Tow-Steered Composite Cylinders with Cutouts63
Anomaly Detection in Wind Tunnel Experiments by Principal Component Analysis63
Estimate of Temperature Gradients of Thin-Walled Structures Under Thermomechanical Fatigue Loading55
Detecting Under-Resolved Flow Physics Using Supervised Machine Learning49
Radio Communication Blackout Mitigation: Analyzing Magnetic Field Effects via Ray-Tracing Analysis49
Direct Numerical Simulation of High-Enthalpy Turbulent Boundary-Layer Flow with Light Gas Injections46
Line-of-Sight Jitter for Advanced Tactical Laser46
Three-Dimensional Accurate Geometric Modeling and Mechanical Analysis of Wire Mesh for Deployable Antennas45
Numerical Investigation on Combustion-Enhancement Strategy in Shock–Fuel Jet Interaction42
Blending of Reynolds Stress Transport Model and γ Transition Model39
Analytical Modeling for Flapping Wing Deformation and Kinematics with Beam Flexibility39
Active Vibration Control of Flexible Structures with Super-Coiled Actuators38
Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature Flows38
Development of a Low-Noise and High-Efficiency Propeller Using Divergent Riblet Surface Pattern38
Hypersonic Boundary-Layer Receptivity over a Blunt Cone to Freestream Pulse Disturbances37
Numerical Study of Aerodynamic Characteristics of No-Swinging and Free-to-Swing Cross Parachute32
HTPB Heat of Formation: Literature Survey, Group Additive Estimations, and Theoretical Effects32
Revised USM3D-ME Implementation of Negative Version of Spalart–Allmaras Turbulence Model32
Efficient Nonlinear Aeroservoelastic Modeling for Morphing Wing with Bilinear Stiffness31
Low-Reynolds Number Behavior of the Leading-Edge Suction Parameter at Low Pitch Rates31
Feature Selection, Clustering, and Prototype Placement for Turbulence Datasets31
Supersonic Freestream Density Fluctuations from Focused Laser Differential Interferometry and Pitot-Probe Measurements29
Distortion Control in Intakes Subject to Strong Crosswinds Using Steady Vortex Generator Jets29
Adaptive High-Order Fluid-Structure Interaction Simulations with Reduced Mesh-Motion Errors29
Excellence in Publications - Revisited29
Control of Flow Structures on Nonslender Delta Wing Utilizing Nozzle-Type Bleeding Slots28
Shock Propagation Through a Square Injector: Investigation into Rotating-Detonation Engine Injector Dynamics28
Rigid–Flexible Coupled Modeling and Flexoelectric Control for Flexible Rotating Structures28
Parametric Model Order Reduction for Structural Optimization of Fiber Composite Structures28
Analytical Linearization of Aerodynamic Loads in Unsteady Vortex-Lattice Method for Nonlinear Aeroelastic Applications27
Influence of Time-Varying Freestream Conditions on the Dynamics of Unsteady Boundary-Layer Separation27
Rapid Prediction of Compressor Rotating Stall Inception Using Arnoldi Eigenvalue Algorithm26
Validated Dynamic Stall Simulation of Pitching Low Reynolds Number Airfoils26
Quasi-Conical Free Interaction in Fin-Induced Shock Wave/Laminar Boundary-Layer Interactions26
Adjoint-Free Aerodynamic Shape Optimization of the Common Research Model Wing25
Computer-Graphics-Based Optical Tracking for Hypersonic Free-Flight Experiments25
Characteristics of Combined-Cycle Inlet During Mode Transition in Off-Design State24
Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts24
On the Use of Power-Based Parameters for Blowing Active Flow Control Systems23
Conceptual Demonstration of Hydrogen Peroxide Based Electrochemical Propulsion with Rotating Gliding Arc23
Momentum Coefficient Governing Discrete Jet Actuation for Separation Control23
Convolution for Haystacking in Turbulence-Ingesting Rotor Noise23
Hybrid Learning Approach to Sensor Fault Detection with Flight Test Data23
Propeller Ground Effect in Forward Flight23
Panel Aeroelastic Stability in Irregular Shock Reflection22
Method for Controlling Vibration and Harvesting Energy by Spacecraft: Theory and Experiment22
Transient Invisibility and Cloak of Impact Elastic Wave in Piezoelectric/Piezomagnetic Metamaterials22
Nonlinear Oscillations and Stability of Rotating Low-Aspect-Ratio Blades Containing Internal Resonance22
Wall-Modeled Large-Eddy Simulation of Turbulent Boundary Layer with Spatially Varying Pressure Gradients22
Simple, Fast Nitric Oxide Planar Laser-Induced Fluorescence Model for Computational Fluid Dynamics Applications22
Adaptive Selection of Decomposed Function Information Sources for Rapid Neural Networks22
Time-Domain Boundary Element Method with Broadband Impedance Boundary Condition22
Experimental Investigation of Flow and Noise Control by Porous Coated Tandem Cylinder Configurations22
Double Peak-Heating in Hypersonic Transitional Shock-Wave/Boundary-Layer Interactions21
Output-Based Adaptive Reynolds-Averaged Navier–Stokes Higher-Order Finite Element Solutions on a Multielement Airfoil21
Improved Finite Element Method for Inflated Beams with Local Wrinkles21
Identification of Discrete Tonal Noise in Inclined Jet Impingement Using Pressure-Sensitive Paint21
Higher-Order Approximations for Stabilizing Zero-Energy Modes in Non-Ordinary State-Based Peridynamics Models21
Direct Numerical Simulation of a Turbulent Boundary Layer over Acoustic Liners21
Design Methods for Variable-Stiffness Super-Ellipsoidal Pressure Vessels Under Thermomechanical Loading20
Arbitrary-Order Sensitivity Analysis in Wave Propagation Problems Using Hypercomplex Spectral Finite Element Method20
Fluid/Structure Interaction of Cantilevered Plate in Supersonic Separated Flow20
Coupled-Mode Versus Single-Degree-of-Freedom Flutter: The Third Parameter in Flutter20
Potential for Dynamic Instability of Flow in Simplified Wind Tunnel20
Kiel Probes for Stagnation Pressure Measurement in Rotating Detonation Combustors19
Application of Time-Variant Systems Theory to the Unsteady Aerodynamics of Rotary Wings19
Flutter and Limit-Cycle Oscillations of a Panel Using Unsteady Potential Flow Aerodynamics19
Unsteady Pressure Gradients in Wind Tunnels with Time-Varying Freestreams19
Transonic Flutter of Skin Panels Pinned at the Center19
Method for Reduced-Order Modeling with Mode Selection Criterion18
Enhancing Lattice Kinetic Schemes for Fluid Dynamics with Lattice-Equivariant Neural Networks18
Dynamically Linearized Time-Domain Approach for Limit-Cycle Oscillation Prediction for an Elastic Panel18
Experimental Investigation of a Small Drone Propeller Aerodynamics in Forward Flight18
Adjoint-Based Design Optimization of Stability Constrained Systems18
Shock Oscillation Mechanism of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions18
Multi-Objective Optimization for Curvilinearly Stiffened Porous Sandwich Plates Reinforced with Graphene Nanoplatelets18
Numerical Simulation of Circulation Control for a Wing Section Using Coanda Jets18
Noise from a Model-Scale Vertical-Axis Wind Turbine17
Unsteady Flow Transition Effects on a Transonic Laminar Airfoil17
Optimal Sensor Placement for Azimuthal Acoustic Modes in Cylindrical Ducts17
Basic Research Perspective on Quantum Information Science for the Aerospace Community17
Wall-Resolved Large-Eddy Simulation of Flow over a Parametric Set of Gaussian Bumps17
Parameterized Fictitious Mode of Morphing Wing with Bilinear Hinge Stiffness17
Cyclostationary Analysis of Fan Noise Influenced by an Inflow Control Device17
Effects of Dilution and Pressure on Detonation Propagation Across an Inert Layer17
Foreign Object Impact Analysis–Assisted Certification Studies for On-Demand Mobility Aircraft17
Measurements of T5 Shock Tunnel Freestream Temperature, Velocity, and Composition17
Arch Vortex in Flow over a Three-Dimensional Gaussian Bump17
Effect of Plasma-Enhanced Low-Temperature Chemistry on Deflagration-to-Detonation Transition in a Microchannel17
Effects of Reynolds Number and Protuberance Amplitude on Twin-Protuberance Airfoil Performance17
Absolute Nodal Coordinate Formulation-Based Shape Sensing Approach for Large Deformation: Plane Beam17
Durability of Buckled Composites Using Virtual Crack Closure Technique Fatigue R-Curve Implementation17
A Conditional Perspective of the Ship Airwake17
Fully Parabolized Hypersonic Sonic Boom Prediction with Real Gas and Viscous Effects17
Multiswept Wing Planform Study at Subsonic, Transonic, and Supersonic Speeds16
Unsteady Aerodynamics Around a Pitching Airfoil with Shock and Shock-Induced Boundary-Layer Separation16
Nonlinear Nonmodal Analysis of Hypersonic Flow over Blunt Cones16
Full-Span Topology of Trailing-Edge Separation at Different Angles of Attack16
Unsteady Propagation and Mean Corrections in Open-Jet and Kevlar® Wind Tunnels16
High-Fidelity Gradient-Based Wing Structural Optimization Including Geometrically Nonlinear Flutter Constraint16
Reynolds-Stress Model Computations of NASA Juncture Flow Experiment16
Linear and Nonlinear Disturbance Evolution on the Frustum of Hypersonic Ogive Cylinders16
Multiscale Reduced-Order Modeling of a Titanium Skin Panel Subjected to Thermomechanical Loading16
Transition to Weak-Shock Solution Around Centerbody Using Laser Energy Deposition16
Flat-Plate Turbulent Skin Friction Response to Rapid Temporal Freestream Variations16
Flowfield Analysis of Vortex Interactions During Large Sharp-Edged Gusts16
Highly Efficient Wall-Distance-Based Parallel Unstructured Overset Grid Assembly15
Hypersonic Boundary-Layer Transition on Cold-Wall Canonical Geometries with Quantified Distributed Roughness Elements15
Nonlinear Aeroelastic Reduced Order Modeling with Optimized Sparse Multi-Input Volterra Kernels15
Ejecta from Granular-Medium Cratering by a Supersonic Jet Entering a Continuum Atmosphere15
Design of Fluidic Injector for Supersonic Jet Manipulation15
Aeroelastic Simulation and Experimental Validation of a 3D-Printed Passive Morphing Airfoil15
Laminar Separation Bubble Noise on a Propeller Operating at Low Reynolds Numbers15
Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry15
Aeroelastic Response of a Z-Shaped Folding Wing During the Morphing Process15
Aeroelastic Wing Performance in High-Intensity Freestream Turbulence: Integral Length Scale Effects15
Vortex Interaction Characteristics of Multiswept Wings at Subsonic Speeds15
Certified Interval Model Updating Using Scenario Optimization15
Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates15
Aerodynamic Interactions of Side-by-Side Rotors in Ground Proximity15
Effect of Two-Dimensional Short Rectangular Indentations on Hypersonic Boundary-Layer Transition15
Quantum Networks: A New Platform for Aerospace15
Hypersonic Conical Shock-Wave/Turbulent-Boundary-Layer Interaction at High Reynolds Number15
Concave Bump for Impinging-Shock Control in Supersonic Flows15
Transition to Limit-Cycle Oscillation in Fluid-Structure Interactions: Mutual Correlations and Causal Dependencies14
Analysis of Sputtering Yield Measurements for Ion Thruster Grid Materials14
A Thread-Safe Lattice Boltzmann Model for Multicomponent Turbulent Jet Simulations14
Material Response Modeling of Melt Flow-Vapor Ablation for Iron14
On the Dispersion Mechanism of the Flutter Boundary of the AGARD 445.6 Wing14
Rigid-Foldable Polyhedral Origami14
Analytical Method of Evaluating Nonuniformities in Shock Tube Flows: Application14
Mitigation of Roughness-Induced Boundary-Layer Transition on Airfoils Using Shielding Strips14
Control of Reverse Flow over Cantilevered Swept Blades Using Passive Camber Morphing14
Low-Reynolds-Number Aerodynamic Characteristics of Airfoils with Piezocomposite Trailing Surfaces14
Flow and Performance Characterization of Rotating Detonation Combustor Integrated with Various Convergent Nozzles14
Equivalent Load Identification and Verification in Frequency Domain for Liquid Rocket Engine14
Fast Full-Field Simulation of Sonic Boom Using a Space Marching Method14
Flow and Noise Characteristics of Blunt-Trailing-Edge Flat Plate with an Upstream Cylinder14
Effects of Freestream Eddies on Triangular Airfoils for Martian Rotorcraft14
Prediction of Transonic Buffet Aerodynamic Noise Using Multi-Expert Feature Fusion Network14
Multibody Dynamics Modeling and Simulation of Supersonic Flexible Rocket Sled-Track Systems14
Particle Image Velocimetry and Total Temperature Characterization of Arc-Heated Mach 4.5 Free Jet14
Hypersonic Boundary-Layer Receptivity over Circular Cones with Ellipsoidal/Spherical Noses14
Reduced-Order Prediction of Unsteady Propeller Loading and Noise from Pylon Wake Ingestion14
Investigations on Turbulence Model Uncertainty for Hypersonic Shock-Wave/Boundary-Layer Interaction Flows14
Lagrange Multiplier-Based Optimal Control Technique for Streak Attenuation in High-Speed Boundary Layers14
Active Flow Control of Supersonic Jet Using Streamwise Pulsed Blowing14
Plasma-Based Dynamic Stall Control and Modeling on an Aspect-Ratio-One Wing14
Analytical Corrections for Acoustic Transmission in Kevlar-Walled Wind Tunnels13
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning13
An Explicit Algebraic Stress-Based Delayed Detached Eddy Simulation Model for Turbulent Flows13
Variable-Fidelity Euler–Lagrange Framework for Simulating Particle-Laden High-Speed Flows13
Primary Parameters of Swirl Decay in Turbulent Swirling Flows Inside Annular Pipes13
Surface Reconfiguration Method of Mesh Antennas by Electrical Performance13
On the Use of Lifting Line Approaches for Propellers with Large Chord Variations13
Wall Distance Effects on Transition to Turbulence in Low-Reynolds-Number Separated Flows13
Timoshenko Theory Solution for the Debond Characteristics of Sandwich Single-Cantilever-Beam Specimens13
Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow13
Experimental Characterization of Supersonic Diamond Jet Acoustics13
Data-Driven Balanced Truncation for Predictive Model Order Reduction of Aeroacoustic Response13
Stabilisation of Hydrodynamic Instabilities by Critical Layers in Acoustic Lining Boundary Layers13
Calibration of an Extended Eddy Viscosity Turbulence Model Using Bayesian Update13
Stable Dynamic Mode Decomposition Algorithm for Noisy Pressure-Sensitive-Paint Measurement Data13
Machine Learning Aided Low-Order Predictions of Fan Stage Broadband Interaction Noise13
Aeroelastic Simulation of High-Aspect Ratio Wings with Intermittent Leading-Edge Separation13
Analytical Model of Transpired-Coolant Concentration at Downstream Wall in High-Speed Laminar Flow13
Blunt Nose Airfoils for Improved Stall Performance and Transonic Aerodynamics13
Free-Air Simulation Sensitivities on NASA’s High-Lift Common Research Model13
Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection13
Multichannel Plasma Synthetic Jet Actuator Driven by Marx High-Voltage Generator13
Efficiency-Optimal Rigidity Configuration of Passive Torsional Flapping Wings13
Wall-Modeled Large Eddy Simulation of High Speed Flows13
Start-Up Analysis of a Hypersonic Short-Duration Facility13
Quasi-Global Sensitivity Analysis of Supersonic Computational Fluid Dynamics Simulations13
Wind Tunnel Testing of a Passive Gust Load Alleviation Spoiler12
High-Order Spectral/hp-Based Solver for Compressible Navier–Stokes Equations12
Megahertz-Rate Imaging of Hypersonic Boundary-Layer Instabilities in a Mach 10 Shock Tunnel12
Aircraft Engine Surge-Precursor Detection and Antisurge Control Method at Onboard Environment12
Improved Dynamic Geometry Control Algorithms for Efficient Aerodynamic Shape Optimization12
Generalized Background Vector Method for Tailored Three-Dimensional Nonperiodic Woven Composite Designs12
Embedded Parameter Information in Conditional Generative Adversarial Networks for Compressor Airfoil Design12
Effects of Turbulence on NACA 0012 Airfoil Performance at Low Reynolds Number12
Efficient Parallel Dynamic Overset Unstructured Grid for Flow Simulation with Moving Bodies12
Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics at Transonic Conditions12
Investigating Shear-Layer Instabilities in Supersonic Impinging Jets Using Dual-Time Particle Image Velocimetry12
Numerical Analysis of Wave Characteristics in a Methane-Oxygen Rotating Detonation Engine12
Influence of Transverse Normal Strain on Buckling and Vibration of Sandwich Plates12
Moving Morphable Multi Components Introducing Intent of Designer in Topology Optimization12
Data-Driven Approach to the Development of an Aeroelastic Flutter Precursor12
Modification of the Eddy Viscosity Based on the Wall Law at Adverse Pressure Gradient12
Experimental Analysis of Pressure Shielding Mechanisms in Bioinspired Unidirectional Canopies12
Gradient-Free Aeroacoustic Shape Optimization Using Large Eddy Simulation12
Quantifying How Turbulence Enhances Boundary Layer Skin Friction and Surface Heat Transfer12
Theory, Method, and Analysis of Waveriding-Dependent Area12
Optimal Position and Angle of Jet Control for Transonic Shock Buffet with Resolvent Analysis12
Spontaneous Laminar Separation Bubble Bursting on an Airfoil12
Modal Analysis of Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interaction Unsteadiness12
Active Feedback Control on Sound Transmission Loss of Metamaterial Shell12
Surrogate Modeling Accelerated Shape Optimization of Deployable Composite Tape-Spring Hinges12
Fluidic Oscillator with Active Phase Control12
Improved Nonlinear Analysis of a Propeller Blade Based on Hyper-Reduction11
Method for Efficient Evaluation of Temperature Using the NASA Polynomials11
Investigation of Combustion Structure and Flame Stabilization in an Axisymmetric Scramjet11
Verification and Scalability of Mixed-Element USM3D for Benchmark Three-Dimensional Flows11
Scaling Analysis on the Dynamic and Instability Characteristics of Isolated Wingtip Vortex11
Control of Various Swept Shock-Wave Interactions Using Corotating Vortex Generators11
Parameterizing Airfoil Shape Using Aerodynamic Performance Parameters11
System-Level Optimization of Passive Energy Balancing11
Supersonic Aerothermoelastic Experiments of Aerospace Structures11
Design and Fabrication of Submillimeter Supersonic Wind Tunnels for Pressure Measurements11
Local Correlation-Based Transition Model for High-Speed Flows11
On Machine-Learning-Aided Two-Scale Solution for Turbulent Fluid Flows11
Relation Between Geometry and Wake Characteristics of a Supersonic Microramp11
Peregrine Falcon’s Dive: Pullout Maneuver and Flight Control Through Wing Morphing11
Uncertainty Quantification Across Design Space Using Spatially Accurate Polynomial Chaos11
Leading-Edge Cone Method for Waverider Design11
Unsteady Flow Transition Effects on a Pitching Transonic Laminar Airfoil11
Finite Element Modeling of Rigid-Flex Printed-Circuit-Board Origami Robotics Subjected to Large-Scale Deformations11
Compact High-Order Gas-Kinetic Scheme for Three-Dimensional Flow Simulations11
Simultaneous Shadowgraph and CH* Chemiluminescence of a Flow-Through Rotating Detonation Combustor11
Energy Harvesting and Propulsion of Pitching Airfoils with Passive Heave and Deformation11
Data-Driven Method for Flow Sensing of Aerodynamic Parameters Using Distributed Pressure Measurements11
Optimal Strategy of Tridirectional Graphene Nanoplatelet Reinforcement for Functionally Graded Sandwich Structures11
2022 Editorial: Advancing Aerospace Sciences and Engineering11
Buckling and Prestressed Vibrations of Periodic Nonprismatic Beams Using Integral Equation Approach11
Physics-Informed Acoustic Liner Optimization: Balancing Drag and Noise11
Automatic Shock Detection, Extraction, and Fitting in Schlieren and Shadowgraph Visualization11
Diaphragm-Induced Attenuation in Shock Tubes11
Radiative Coefficients and Their Influence on In-Depth Heating of Porous Ablators11
Trailing-Edge Noise Comparability in Open, Closed, and Hybrid Wind Tunnel Test Sections11
Description and Prediction of Roughness-Induced Transition in Swept-Wing Boundary Layers11
Computations of Side Loads in a Thrust-Optimized Parabolic Nozzle During High-Altitude Testing11
Uncertainty Analysis in Airfoil–Turbulence Interaction Noise Using Polynomial Chaos Expansion11
New Methodology for Robust-Optimal Design with Acceptable Risks: An Application to Blended/Wing/Body Aircraft11
Numerical Investigation of Aeroelastic Characteristics of Grid Fin11
Theory of Machine Learning Assisted Structural Optimization Algorithm and Its Application11
Control of Dynamic Stall on Swept Finite Wings10
Multifidelity Methodology for Reduced-Order Models with High-Dimensional Inputs10
Comparability of Inflow Turbulence Distortion for Airfoil and Cylinder10
Reviews and Challenges in Reliability Design of Long March Launcher Control Systems10
High-Fidelity Aircraft Simulations for the Application in an Industrialized Ditching Analysis Process10
Dynamic Model Reduction for Viscously Damped Structures with Statically Determinate Interfaces10
Microstructure-Sensitive Stochastic Design of Polycrystalline Materials for Quasi-Isotropic Properties10
Experimental Investigations of Failure Behavior for Aerogel-Cored Stitched Sandwich Composites Under Vibration Conditions10
Boundary-Layer Instabilities over a Cone–Cylinder–Flare Model at Mach 610
Multispecies Flow Indirect-Noise Modeling Re-Examined with a Helicopter-Engine Application10
Stress and Failure Onset Analysis of Thin Composite Deployables by Global/Local Approach10
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