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 2022-05-01 to 2026-05-01.)

Article	Citations
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability	161
Editorial Board	140
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow	137
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance	105
Optimal guidance laws for diffractive solar sails with Littrow transmission grating	105
Buckling optimization of non-uniformly distributed curved grid-stiffened helicoidal composite panels with cutouts	100
Nonlinear damping model for supersonic air-intake buzz	87
Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models	86
Mode switching in fluidic oscillators from feedback channel length variation	84
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft	84
Conjugate heat transfer analysis on return-flow impingement cooling scheme applied to aeroengine turbine blade leading edge	82
Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet	77
A vector-type finite-time trajectory tracking controller for quadrotor UAVs with safety constraints	74
Computational aeroacoustic study of co-rotating rotors in hover	72
Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle	72
Breakdown of boundary layer instabilities on a straight cone in a hypersonic shock tunnel	71
Adaptive attitude tracking control for reusable launch vehicle with actuator and sensor faults	71
Weight-adaptive augmented Lagrange multiplier sequential convex programming for nonlinear trajectory optimization	68
Investigation on premixed spherical hydrogen-air flame development, turbulence characteristics and NOx emission in porous media with different pellets sizes	68
Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation	68
Experimental investigation on the effects of transverse injection distribution scheme on dual flame dynamics subjected to flow disturbances	66
Multi-Unit hybrid modeling method and nonlinear dynamics analysis of the whole aero-engine system	62
Numerical study of unsteady flow and cooling characteristics of turbine blade cutback trailing edges integrated with pin fins and film holes	62
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]	61
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance	60

Tension-twist coupling morphing wing using a novel mechanical metamaterial	60
Effect of cavity depth on air-breathing rotating detonation engine fueled by liquid kerosene	59
Disturbance observer-based fractional-order sliding mode control for free-floating space manipulator with disturbance	57
Numerical study of hydrogen ratio effect on detonation initiation characteristics of aviation kerosene with hydrogen addition	57
Fixed-time attitude control for hypersonic morphing vehicles: A dynamic memory event-triggering approach	57
A three-dimensional collision avoidance strategy for multiple unmanned aerial vehicles using velocity obstacle method	56
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle	56
Low-velocity impact simulation of carbon fiber reinforced composite laminate using IFF-criterion based on BP-ANN	56
Adaptive hybrid Kalman filter for attitude motion parameters estimation of space non-cooperative tumbling target	56
Research on the cooling performance and thermal stress characteristic of turbine blade with typical array film holes	55
Parameter correction and ground testing of large-scale space structure	54
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification	54
Three-dimensional practical cooperative guidance law for salvo attack considering velocity variation	54
Predefined-time disturbance observer-based formation control for aerial-ground heterogeneous multi-agent systems under quantitative prescribed performance constraints	54
Multi-objective aerodynamic optimization of an axisymmetric variable-geometry inlet with a Mach 5 design point	54
A robust adaptive linear parameter-varying gain-scheduling controller for aeroengines	54
Wind effects on urban air mobility noise during landing procedures	54
The FFD parametric method based on streamline for three-dimensional inward-turning inlet	53
A review of aircraft subsonic and supersonic combustors	53
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities	53
Design and analysis of buckling-induced honeycombs with tailorable out-of-plane crushing performance	53
Event-triggered attitude control for hypersonic morphing vehicles using fixed-time control technique	53
Numerical study on the internal flow mechanisms of variable geometry high-load low-pressure turbine cascade under wide operating conditions	53
Large eddy simulation on the interaction effect of shock waves induced by wall ramps on strut flame	52
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure	52
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure	52
Three-dimensional spatial-temporal cooperative guidance enhanced by physically-guided neural networks	51
Optimizing unmanned aerial vehicle aerodynamics: a two-stage approach using genetic algorithms and adjoint methods	51
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade	51