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 2020-11-01 to 2024-11-01.)

Article	Citations
Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines	116
Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization	87
Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks	79
Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach	56
Improved Amplification Factor Transport Transition Model for Transonic Boundary Layers	55
Supersonic and Hypersonic Drag Coefficients for a Sphere	55
Numerical Study on JP-10/Air Detonation and Rotating Detonation Engine	55
Data-Driven Aerospace Engineering: Reframing the Industry with Machine Learning	52
Analysis of the Detonation Wave Structure in a Linearized Rotating Detonation Engine	50
Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions	48
Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers	45
Learning the Aerodynamic Design of Supercritical Airfoils Through Deep Reinforcement Learning	41
Double–Double: New Family of Composite Laminates	39
Propulsion Performance of Cylindrical Rotating Detonation Engine	39
Sound Propagation of Three-Dimensional Sandwich Panels: Influence of Three-Dimensional Re-Entrant Auxetic Core	38
General Drag Coefficient for Flow over Spherical Particles	36
Complex Standard Eigenvalue Problem Derivative Computation for Laminar–Turbulent Transition Prediction	35
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data	35
Experimental Aeroelastic Benchmark of a Very Flexible Wing	34
Experimental and Numerical Crashworthiness Study of a Full-Scale Composite Fuselage Section	33
Control of Shock-Induced Separation of a Turbulent Boundary Layer Using Air-Jet Vortex Generators	33
Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination	32
Investigation of Combustion Characteristics in a Kerosene-Fueled Supersonic Combustor with Air Throttling	31
Measurements of Reflected Shock Tunnel Freestream Nitric Oxide Temperatures and Partial Pressure	30
Fast Predictions of Aircraft Aerodynamics Using Deep-Learning Techniques	29

Effect of Transverse Gust Velocity Profiles	29
Smart Solar Array Consisting of Shape-Memory Releasing Mechanisms and Deployable Hinges	28
Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer	28