AIAA Journal

Papers
(The H4-Index of AIAA Journal is 27. 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
Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry87
Direct Eigenstructure Assignment for Model Updating80
Flow Dynamics of a Contra-Rotating Axial Fan Under Windmilling and Locked Conditions63
Shock Propagation Through a Square Injector: Investigation into Rotating-Detonation Engine Injector Dynamics61
Multi-Objective Reverse Design and Pattern Analysis of Solid Propellant Grains61
Conformally Decambered Natural Laminar Flow Blades for Vertical-Axis Wind Turbines61
Distortion Control in Intakes Subject to Strong Crosswinds Using Steady Vortex Generator Jets48
Robust Equivalent Source Method Based on Filtered Pressure for Aerodynamic Sound Prediction47
Energy-Preserving Perturbation Method for Thermally Induced Dynamics in Aerospace Tensegrity Structures45
Lattice Boltzmann Formulation for Eight-Wave Magnetohydrodynamics45
Comparing Discontinuous Galerkin Shock-Capturing Techniques Applied to Inviscid Three-Dimensional Hypersonic Flows44
Simulation of Atmospheric Boundary Layer for Air Inlet Testing in Crossflow43
Deflected Synthetic Jet due to Vortices Induced by a Tri-Electrode Plasma Actuator42
Identifying the Self-Sustaining Mechanisms of Transonic Airfoil Buffet with Resolvent Analysis39
Modeling of Transonic Transitional Three-Dimensional Flows for Aerodynamic Applications35
Robust Dynamic Mode Decomposition Methodology for an Airfoil Undergoing Transonic Shock Buffet34
SPARK: Implicit Time-Accurate Algorithm for All-Speed Viscous Flows33
Gradient-Based Optimization of Chaotic Panel Flutter33
Novel High-Precision and Efficient Momentum Source Method32
Enhancing the Power-Extraction Efficiency of a Flapping Foil by Active Morphing32
Pneumatic-Probe Measurement Errors Caused by Fluctuating Flow Angles29
High-Performance Froth Singlet Oxygen Generator29
Post-Impact Fatigue Durability Assessment of Composite Laminates for Enhanced Aircraft Sustainment29
Adjoint-Free Aerodynamic Shape Optimization of the Common Research Model Wing29
Database Development and Component Design with Two-Dimensional Trusslike Microstructures28
Links Between Steepened Mach Waves and Coherent Structures for a Supersonic Jet28
Momentum Coefficient Governing Discrete Jet Actuation for Separation Control27
Efficient Global Optimization of Advanced Drop-Hinged Flap27
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