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 2021-05-01 to 2025-05-01.)

Article	Citations
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	166
A trajectory optimization method for reducing magnetic disturbance of an internal combustion engine powered unmanned aerial vehicle	124
Editorial Board	118
Visualization of over-expanded supersonic wall-jet	114
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	112
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	103
Nonlinear damping model for supersonic air-intake buzz	102
Development of maximum conical shock angle limit for osculating cone waveriders	91
Experimental study of high-speed air intake performance by side clearance	87
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance	86
Optimal guidance laws for diffractive solar sails with Littrow transmission grating	85
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	85
Parameter Correction and Ground Testing of Large-scale Space Structure	84
Tension-twist coupling morphing wing using a novel mechanical metamaterial	83
Seal dynamics of supercritical carbon dioxide turbine with the uncertain rotor nonlinear motion	80
Experimental investigation of the characteristics of direct injection nozzle sprays in an afterburner environment	79
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	76
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	75
Line sampling based fuzzy simulation coupled with adaptive Kriging for estimating failure possibility of simplified turbine disk	75
Efficient fuzzy simulations for estimating the failure credibility of engineering structures under fuzzy environment	75
Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network	71
Adaptive super-twisting trajectory tracking control for an unmanned aerial vehicle under gust winds	70
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	69
Cooperative integrated guidance and control design for simultaneous interception	68
Numerical study of back-propagation suppression and intake loss in an air-breathing pulse detonation engine	68

Chebyshev-series solutions for nonlinear systems with hypersonic gliding trajectory example	66
A real-time fault diagnosis method for hypersonic air vehicle with sensor fault based on the auto temporal convolutional network	65
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle	63
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	63
On flight instabilities of capsule-rigid parachute system during supersonic planetary descent	63
Numerical study of the aerodynamic effects of bio-inspired leading-edge serrations on a heaving wing at a low Reynolds number	62
Effects of propeller separation and onset flow condition on the performance of quadcopter propellers	62
On the control allocation of fully actuated multirotor aerial vehicles	60
Fixed-time attitude control for hypersonic morphing vehicles: A dynamic memory event-triggering approach	60
Experimental investigation on the effects of transverse injection distribution scheme on dual flame dynamics subjected to flow disturbances	59
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure	59
Multiobjective optimization of a staggered-rotor octocopter design based on a surrogate model	58
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft	58
Preliminary study on pulsed jets with three-dimensional effects for flow separation control in a compressor blade	57
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	57
Theoretical and numerical analysis of effects of sudden expansion and contraction on compressible flow phenomena in Hyperloop system	56
Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation	55
Adaptive hybrid Kalman filter for attitude motion parameters estimation of space non-cooperative tumbling target	55
Unknown input observer-based appointed-time funnel control for quadrotors	54
Optimization-based iterative and robust strategy for spacecraft relative navigation in elliptical orbit	53
Twin-fuselage configuration for improving fuel efficiency of passenger aircraft	53
Design and analysis of buckling-induced honeycombs with tailorable out-of-plane crushing performance	53
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump	53
Large Eddy Simulation of cavity stabilized ramjet combustion	52
Three-dimensional pore-scale study of the directional heat transfer in a high thermal conductivity carbon/carbon composite protection system	52
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade	52
Experimental and computational investigation of stacked rotor performance in hover	52
Boundary layer suction timing and location effects on unstarting flows in a model scramjet	52
Extended fuzzy first-order and second-moment method based on equivalent regularization for estimating failure credibility	52