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 2021-11-01 to 2025-11-01.)

Article	Citations
Weight-adaptive augmented Lagrange multiplier sequential convex programming for nonlinear trajectory optimization	199
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	143
Experimental investigation of the characteristics of direct injection nozzle sprays in an afterburner environment	138
Development of maximum conical shock angle limit for osculating cone waveriders	117
A vector-type finite-time trajectory tracking controller for quadrotor UAVs with safety constraints	111
Discovery, interpretation, and model-based judgment of a hidden operating condition during the process from compressor stall to surge induced by inlet distortion	108
Numerical study on the internal flow mechanisms of variable geometry high-load low-pressure turbine cascade under wide operating conditions	103
Line sampling based fuzzy simulation coupled with adaptive Kriging for estimating failure possibility of simplified turbine disk	102
A review of aircraft subsonic and supersonic combustors	100
Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition	98
Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network	97
A robust adaptive linear parameter-varying gain-scheduling controller for aeroengines	97
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance	87
Parameter correction and ground testing of large-scale space structure	86
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	83
Numerical analysis of the performance and drag reduction mechanisms of outboard horizontal stabilizers	82
Seal dynamics of supercritical carbon dioxide turbine with the uncertain rotor nonlinear motion	80
Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet	80
Adaptive attitude tracking control for reusable launch vehicle with actuator and sensor faults	78
Efficient fuzzy simulations for estimating the failure credibility of engineering structures under fuzzy environment	76
Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models	76
Computational aeroacoustic study of co-rotating rotors in hover	75
Cooperative integrated guidance and control design for simultaneous interception	74
Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation	74
Dynamic modeling and parametric instability analysis of internally damped rotating composite shafts in inertial and rotating frames	73

On flight instabilities of capsule-rigid parachute system during supersonic planetary descent	69
Nonlinear damping model for supersonic air-intake buzz	68
An integrated imitation and reinforcement learning methodology for robust agile aircraft control with limited pilot demonstration data	67
Buckling optimization of non-uniformly distributed curved grid-stiffened helicoidal composite panels with cutouts	66
Fixed-time attitude control for hypersonic morphing vehicles: A dynamic memory event-triggering approach	66
Unknown input observer-based appointed-time funnel control for quadrotors	65
Editorial Board	64
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	64
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle	62
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	61
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	61
Event-triggered attitude control for hypersonic morphing vehicles using fixed-time control technique	59
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	57
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	57
Effects of propeller separation and onset flow condition on the performance of quadcopter propellers	57
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure	57
Experimental study of high-speed air intake performance by side clearance	55
Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle	55
Reinforcement learning strategy for spacecraft attitude hyperagile tracking control with uncertainties	54
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft	54
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump	54
Extended fuzzy first-order and second-moment method based on equivalent regularization for estimating failure credibility	53
Prescribed finite-time boundary control of constrained flexible satellite systems with translational motion modeling	53
Theoretical and numerical analysis of effects of sudden expansion and contraction on compressible flow phenomena in Hyperloop system	53
A real-time fault diagnosis method for hypersonic air vehicle with sensor fault based on the auto temporal convolutional network	53
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	53
Numerical study of the aerodynamic effects of bio-inspired leading-edge serrations on a heaving wing at a low Reynolds number	53
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	52
Multiobjective optimization of a staggered-rotor octocopter design based on a surrogate model	52