OOIR: Observatory of International Research

Papers

(The H4-Index of Aerospace Science and Technology is 50. 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 2022-01-01 to 2026-01-01.)

Article	Citations
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	149
Buckling optimization of non-uniformly distributed curved grid-stiffened helicoidal composite panels with cutouts	132
Editorial Board	119
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	119
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	111
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	108
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure	107
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	102
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	97
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	94
Optimal guidance laws for diffractive solar sails with Littrow transmission grating	93
Discovery, interpretation, and model-based judgment of a hidden operating condition during the process from compressor stall to surge induced by inlet distortion	92
Experimental study of high-speed air intake performance by side clearance	90
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump	85
Computational aeroacoustic study of co-rotating rotors in hover	82
Breakdown of boundary layer instabilities on a straight cone in a hypersonic shock tunnel	80
A three-dimensional collision avoidance strategy for multiple unmanned aerial vehicles using velocity obstacle method	80
Nonlinear damping model for supersonic air-intake buzz	76
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	75
Optimization-based iterative and robust strategy for spacecraft relative navigation in elliptical orbit	70
Investigation on premixed spherical hydrogen-air flame development, turbulence characteristics and NOx emission in porous media with different pellets sizes	70
Research on the cooling performance and thermal stress characteristic of turbine blade with typical array film holes	70
Assessing the retrieval procedure of complex-valued forces from airborne pressure fields by means of DIC-based full-field receptances in simplified pseudo-inverse vibro-acoustics	68
Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models	67
Numerical analysis of the performance and drag reduction mechanisms of outboard horizontal stabilizers	67

Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation	66
On flight instabilities of capsule-rigid parachute system during supersonic planetary descent	65
Dynamic modeling and parametric instability analysis of internally damped rotating composite shafts in inertial and rotating frames	65
Efficient fuzzy simulations for estimating the failure credibility of engineering structures under fuzzy environment	64
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance	62
Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle	62
Optimizing unmanned aerial vehicle aerodynamics: a two-stage approach using genetic algorithms and adjoint methods	60
On the control allocation of fully actuated multirotor aerial vehicles	60
Multi-objective aerodynamic optimization of an axisymmetric variable-geometry inlet with a Mach 5 design point	60
Numerical study on the aerodynamic performance of ducted fans under free windmilling conditions	59
Unknown input observer-based appointed-time funnel control for quadrotors	57
Anomaly detection in UAV Swarms: An information geometric approach to behavioral analysis	57
Application of the stagnation cavity on V-shaped blunt leading edges for thermal protection	57
Event-triggered attitude control for hypersonic morphing vehicles using fixed-time control technique	56
Effects of propeller separation and onset flow condition on the performance of quadcopter propellers	55
Conjugate heat transfer analysis on return-flow impingement cooling scheme applied to aeroengine turbine blade leading edge	54
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle	54
Large eddy simulation on the interaction effect of shock waves induced by wall ramps on strut flame	53
Wind effects on urban air mobility noise during landing procedures	53
Adaptive attitude tracking control for reusable launch vehicle with actuator and sensor faults	53
Low-velocity impact simulation of carbon fiber reinforced composite laminate using IFF-criterion based on BP-ANN	52
Adaptive hybrid Kalman filter for attitude motion parameters estimation of space non-cooperative tumbling target	51
An integrated imitation and reinforcement learning methodology for robust agile aircraft control with limited pilot demonstration data	51
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft	50
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade	50
Boundary layer suction timing and location effects on unstarting flows in a model scramjet	50
Parameter correction and ground testing of large-scale space structure	50