OOIR: Observatory of International Research

Papers

(The H4-Index of AIAA Journal is 28. 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.)

Article	Citations
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines	91
Efficient Aerodynamic Shape Optimization with Deep-Learning-Based Geometric Filtering	87
Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization	74
Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks	66
Learning Physics-Based Reduced-Order Models for a Single-Injector Combustion Process	62
Hypersonic Fluid–Structure Interactions in Compression Corner Shock-Wave/Boundary-Layer Interaction	54
Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach	48
Analysis of the Detonation Wave Structure in a Linearized Rotating Detonation Engine	46
Numerical Study on JP-10/Air Detonation and Rotating Detonation Engine	45
High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design	44
Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators	44
Supersonic and Hypersonic Drag Coefficients for a Sphere	41
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions	40
Improvements to the Quadratic Constitutive Relation Based on NASA Juncture Flow Data	37
Data-Driven Aerospace Engineering: Reframing the Industry with Machine Learning	37
Quad-Rotor Flight Simulation in Realistic Atmospheric Conditions	36
Propulsion Performance of Cylindrical Rotating Detonation Engine	33
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators	32
Lift Regulation During Transverse Gust Encounters Using a Modified Goman–Khrabrov Model	32
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning	31
Self-Deployable, Self-Stiffening, and Retractable Origami-Based Arrays for Spacecraft	31
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data	31
Sound Propagation of Three-Dimensional Sandwich Panels: Influence of Three-Dimensional Re-Entrant Auxetic Core	30
Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section	30
Correction to the Spalart–Allmaras Turbulence Model, Providing More Accurate Skin Friction	30

Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers	30
A Benchmark Study of Kinetic Models for Shock Waves	29
Experimental Aeroelastic Benchmark of a Very Flexible Wing	28
Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil	28