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 2021-06-01 to 2025-06-01.)

Article	Citations
Editorial Board	168
Experimental study of high-speed air intake performance by side clearance	128
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	122
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	117
Experimental investigation of the characteristics of direct injection nozzle sprays in an afterburner environment	117
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	103
Efficient fuzzy simulations for estimating the failure credibility of engineering structures under fuzzy environment	102
Line sampling based fuzzy simulation coupled with adaptive Kriging for estimating failure possibility of simplified turbine disk	95
Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network	90
Cooperative integrated guidance and control design for simultaneous interception	89
Numerical study of back-propagation suppression and intake loss in an air-breathing pulse detonation engine	87
On flight instabilities of capsule-rigid parachute system during supersonic planetary descent	86
Preliminary study on pulsed jets with three-dimensional effects for flow separation control in a compressor blade	85
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	85
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade	82
Integrated optimization of a high-lift low-pressure turbine cascade based on dynamic support vector regression	82
Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation	82
Boundary layer suction timing and location effects on unstarting flows in a model scramjet	82
Numerical analysis of the performance and drag reduction mechanisms of outboard horizontal stabilizers	75
Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle	75
Experimental investigation on the effects of transverse injection distribution scheme on dual flame dynamics subjected to flow disturbances	71
Event-triggered attitude control for hypersonic morphing vehicles using fixed-time control technique	71
Unknown input observer-based appointed-time funnel control for quadrotors	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	70
Effect of cavity depth on air-breathing rotating detonation engine fueled by liquid kerosene	69

Design and experimental validation of a disturbing force application unit for simulating spacecraft separation	67
Unsteady aerodynamic reduced-order modeling based on machine learning across multiple airfoils	67
Extended fuzzy first-order and second-moment method based on equivalent regularization for estimating failure credibility	67
Multiobjective optimization of a staggered-rotor octocopter design based on a surrogate model	65
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle	63
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	63
Chebyshev-series solutions for nonlinear systems with hypersonic gliding trajectory example	62
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	62
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	60
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure	60
Large Eddy Simulation of cavity stabilized ramjet combustion	60
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	59
Optimal guidance laws for diffractive solar sails with Littrow transmission grating	58
Experimental and computational investigation of stacked rotor performance in hover	58
A trajectory optimization method for reducing magnetic disturbance of an internal combustion engine powered unmanned aerial vehicle	58
Twin-fuselage configuration for improving fuel efficiency of passenger aircraft	57
Computational aeroacoustic study of co-rotating rotors in hover	56
Low-velocity impact simulation of carbon fiber reinforced composite laminate using IFF-criterion based on BP-ANN	56
Development of maximum conical shock angle limit for osculating cone waveriders	55
Multi-objective aerodynamic optimization of an axisymmetric variable-geometry inlet with a Mach 5 design point	54
Optimization-based iterative and robust strategy for spacecraft relative navigation in elliptical orbit	54
Adaptive super-twisting trajectory tracking control for an unmanned aerial vehicle under gust winds	54
Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition	53
On the control allocation of fully actuated multirotor aerial vehicles	53
Tension-twist coupling morphing wing using a novel mechanical metamaterial	52
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance	52
Reinforcement learning strategy for spacecraft attitude hyperagile tracking control with uncertainties	52