OOIR: Observatory of International Research

Papers

(The H4-Index of Aerospace Science and Technology is 52. 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 2022-08-01 to 2026-08-01.)

Article	Citations
Optimization-based iterative and robust strategy for spacecraft relative navigation in elliptical orbit	173
Editorial Board	157
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	149
Optimal guidance laws for diffractive solar sails with Littrow transmission grating	120
Large eddy simulation on the interaction effect of shock waves induced by wall ramps on strut flame	112
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure	107
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	93
Numerical analysis of the performance and drag reduction mechanisms of outboard horizontal stabilizers	91
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	89
Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition	89
Wind effects on urban air mobility noise during landing procedures	82
Low-velocity impact simulation of carbon fiber reinforced composite laminate using IFF-criterion based on BP-ANN	80
Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models	78
The FFD parametric method based on streamline for three-dimensional inward-turning inlet	77
Corrigendum to “Three-dimensional fault-tolerant cooperative guidance law with constraints on relative impact velocity and attack angle” [AESCTE, 168 (2026) 111003]	76
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	73
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	71
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	71
Integrated optimization of a high-lift low-pressure turbine cascade based on dynamic support vector regression	70
Application of the stagnation cavity on V-shaped blunt leading edges for thermal protection	69
Theoretical analysis of nitrogen oxide generation in hydrogen-air rotating detonation combustors based on Lagrangian parcel tracking method	68
Anomaly detection in UAV Swarms: An information geometric approach to behavioral analysis	68
Efficient fuzzy simulations for estimating the failure credibility of engineering structures under fuzzy environment	67
Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network	65
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade	64

Parametric study of lateral jet interaction in diatomic gas non-equilibrium flows using wave-particle method	63
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	63
Improving hypersonic inlet self-starting performance in dual-separation flows using a backward-facing step	63
Comparative aerothermoelastic performance assessment of advanced TPS materials for hypersonic vehicles	63
A Set Theoretic approach for reducing critical load cases in aircraft structural design	61
Experimental research on the atomization of prefilming airblast atomizer under different gravity orientations	61
Adaptive hybrid Kalman filter for attitude motion parameters estimation of space non-cooperative tumbling target	61
Experimental investigation on the effects of transverse injection distribution scheme on dual flame dynamics subjected to flow disturbances	60
Dynamics of vibration mode competition between flutter and forced vibration in thin-walled scramjet isolators under fluctuating backpressure	60
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	59
Mode switching in fluidic oscillators from feedback channel length variation	58
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	58
Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet	58
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft	57
Investigation on premixed spherical hydrogen-air flame development, turbulence characteristics and NOx emission in porous media with different pellets sizes	57
Effects of propeller separation and onset flow condition on the performance of quadcopter propellers	56
Prescribed finite-time boundary control of constrained flexible satellite systems with translational motion modeling	55
Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation	55
An online gas path fault diagnosis for aircraft engine transient behavior based on the residual derivative tracking strategy	55
Kinetic and experimental study of Mn(III) acetylacetonate for green hypergolic ignition in HTP/Kerosene systems	54
High-order positivity-preserving and dissipation-adaptive computational framework with sharp-interface immersed boundaries for high-Mach-number shock-obstacle interactions	53
Optimizing unmanned aerial vehicle aerodynamics: a two-stage approach using genetic algorithms and adjoint methods	53
Fixed-time attitude control for hypersonic morphing vehicles: A dynamic memory event-triggering approach	53
Tube-based nonlinear model predictive control for lateral maneuvering of trans-media vehicle considering planing avoidance	53
Experimental investigation of the characteristics of direct injection nozzle sprays in an afterburner environment	53
Design and analysis of buckling-induced honeycombs with tailorable out-of-plane crushing performance	53
Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation	52
On flight instabilities of capsule-rigid parachute system during supersonic planetary descent	52
Computational aeroacoustic study of co-rotating rotors in hover	52