OOIR: Observatory of International Research

Papers

(The H4-Index of Aerospace Science and Technology is 51. 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.)

Article	Citations
Optimal heliocentric transfers of a Sun-facing heliogyro	159
Effect of dome spacing on flow field and flame dynamics in a three-sector rich-quench-lean combustor	116
Research on multi-hierarchical multi-objective optimization design of scramjet nozzle under geometric constraints	113
Flow simulation of propeller-airframe interaction using a modified blade camber surface loading model	112
Hierarchical pigeon inspired optimization based Multi-UAV obstacle avoidance control	109
Flow field prediction and optimization of non-axisymmetric aero-engine nacelles based on deep learning	101
Model predictive control of a flared folding wingtip for gust load alleviation	100
Fixed-time attitude control of flying-wing unmanned aerial vehicles based on plasma control surface	89
An investigation on bleed flow control of an axisymmetric supersonic intake based on parametric outline optimization design	88
Handling Qualities sizing for aerial vehicles based on control moment polytopes	85
A novel ROM-based FSI model of composite blisk with blades-disk coupling for flutter analysis	84
Research on 3D layered visibility graph route network model and multi-objective path planning for UAVs in complex urban environments	84
Optimization of supersonic combustor configuration based on Gaussian process regression and genetic algorithm	81
Stepwise equivalent modeling for the blisk under nonlinear aerodynamic excitation considering fluid-structure interaction	80
An efficient thermal optimization model with integrated force paths, fully-decomposed hierarchies and hybrid genetic operations for a flight wing	76
Performance of an oxygen-consuming inerting system for an aircraft fuel tank with RP-3 aviation fuel in flight	76
Experimental study on the operational characteristics of a scramjet engine under pressure-varying inflow conditions	76
Online performance seeking control of aero-engine based on stabilization-optimization dual loop	76
Buckling optimization of non-uniformly distributed curved grid-stiffened helicoidal composite panels with cutouts	75
Parameter Correction and Ground Testing of Large-scale Space Structure	75
Low fidelity data driven machine learning based optimisation method for box-wing configuration	71
Aerodynamic optimization of high-lift devices using a 2D-to-3D optimization method based on deep reinforcement learning and transfer learning	70
Numerical simulation of hypersonic reaction flows with nonlinear coupled constitutive relations	69
Dispersion and band gaps of elastic guided waves in the multi-scale periodic composite plates	68
A robust adaptive linear parameter-varying gain-scheduling controller for aeroengines	66

Reentry trajectory planning for hypersonic vehicles via an improved sequential convex programming method	65
Theoretical and numerical analysis of effects of sudden expansion and contraction on compressible flow phenomena in Hyperloop system	65
Disturbance observer-based fractional-order sliding mode control for free-floating space manipulator with disturbance	65
Experimental and computational investigation of stacked rotor performance in hover	64
Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation	64
Geometric mistuning identification and finite element model updating methods for bladed disks	63
Non-axisymmetric aero-engine nacelle design by surrogate-based methods	61
An optimal steering law for sailing with solar and planetary radiation pressure	61
Rebound stabilization for an asteroid lander by flexible plate design	61
Flow characteristics and stability of induced shock waves in the isolator of rotating detonation ramjet under flight Mach number 2.5 conditions	61
Effect of span range of variable-camber inlet guide vane in an axial compressor	59
Event-triggered attitude control for hypersonic morphing vehicles using fixed-time control technique	59
Saturated explicit reference governor for spacecraft constrained attitude reorientation control	58
An improved adaptive Kriging method for the possibility-based design optimization and its application to aeroengine turbine disk	58
Twin-fuselage configuration for improving fuel efficiency of passenger aircraft	58
Influence of upstream wall slope on aerodynamic properties of a rectangular cavity in rarefied hypersonic flows	57
Refined MagSail thrust model for preliminary mission design and trajectory optimization	55
Prescribed finite-time boundary control of constrained flexible satellite systems with translational motion modeling	54
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	54
A deep neural network reduced order model for unsteady aerodynamics of pitching airfoils	53
Heat transfer measurement near injection hole of supersonic nozzle with a sonic jet injection	53
Experimental investigation of wing-propeller aerodynamic interaction in eVTOL configurations	53
Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition	52
Editorial Board	52
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	52
Multi-level and multi-objective structural optimization for hypersonic vehicle design	51
Maneuver mode parametric modeling based on trajectory curve evolution laws for hypersonic glide vehicles	51
Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet	51
Design and compression efficiency analysis of a Mach 0∼4 variable TBCC intake	51