Aerospace Science and Technology

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 2021-09-01 to 2025-09-01.)
ArticleCitations
Editorial Board186
Experimental study of high-speed air intake performance by side clearance132
Corrigendum to “Supercritical wing design based on airfoil optimization and 2.75D transformation” [Aerosp. Sci. Technol. 56 (2016) 168–182]127
Experimental investigation of the characteristics of direct injection nozzle sprays in an afterburner environment109
Experimental study of the combustion characteristic of circular transverse fuel jet in crossflow100
Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network98
Cooperative integrated guidance and control design for simultaneous interception97
Investigation of unsteady flow mechanisms and modal behavior in a compressor cascade96
On flight instabilities of capsule-rigid parachute system during supersonic planetary descent95
Influence of geometric parameters of discrete roughness elements on hypersonic boundary layer instability94
Theoretical and numerical analysis of effects of sudden expansion and contraction on compressible flow phenomena in Hyperloop system90
On the control allocation of fully actuated multirotor aerial vehicles90
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure90
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure82
Fixed-time attitude control for hypersonic morphing vehicles: A dynamic memory event-triggering approach79
Reinforcement learning strategy for spacecraft attitude hyperagile tracking control with uncertainties78
Models of the time-averaged heat release rate of the two-dimensional laminar premixed slit flame subjected to the transverse disturbance77
Experimental investigation on the effects of transverse injection distribution scheme on dual flame dynamics subjected to flow disturbances76
Integrated optimization of a high-lift low-pressure turbine cascade based on dynamic support vector regression74
Seal dynamics of supercritical carbon dioxide turbine with the uncertain rotor nonlinear motion74
Line sampling based fuzzy simulation coupled with adaptive Kriging for estimating failure possibility of simplified turbine disk74
Numerical analysis of the performance and drag reduction mechanisms of outboard horizontal stabilizers73
Preliminary study on pulsed jets with three-dimensional effects for flow separation control in a compressor blade73
Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle69
Nonlinear damping model for supersonic air-intake buzz69
Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet69
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-acoustics69
Parameter correction and ground testing of large-scale space structure66
A vector-type finite-time trajectory tracking controller for quadrotor UAVs with safety constraints65
Low-velocity impact simulation of carbon fiber reinforced composite laminate using IFF-criterion based on BP-ANN64
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump62
A real-time fault diagnosis method for hypersonic air vehicle with sensor fault based on the auto temporal convolutional network62
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle62
Effects of propeller separation and onset flow condition on the performance of quadcopter propellers62
Extended fuzzy first-order and second-moment method based on equivalent regularization for estimating failure credibility61
A trajectory optimization method for reducing magnetic disturbance of an internal combustion engine powered unmanned aerial vehicle61
Chebyshev-series solutions for nonlinear systems with hypersonic gliding trajectory example59
Dynamic bending behavior of double-hat beams filled with alloy hierarchical structure58
An improved reconstruction method of the reflected dynamic pressure in shock tube system based on inverse sensing model identification58
Optimal guidance laws for diffractive solar sails with Littrow transmission grating57
Development of maximum conical shock angle limit for osculating cone waveriders56
Adaptive attitude tracking control for reusable launch vehicle with actuator and sensor faults55
Numerical study of unsteady flow and cooling characteristics of turbine blade cutback trailing edges integrated with pin fins and film holes54
Numerical studies on steady interaction of low enthalpy hypersonic double wedge flows using different gas models54
Learning Chebyshev neural network-based spacecraft attitude tracking control ensuring finite-time prescribed performance54
Design and analysis of buckling-induced honeycombs with tailorable out-of-plane crushing performance53
Observer-based boundary feedback control for attitude tracking of rigid bodies with partially liquid-filled cavities53
Unknown input observer-based appointed-time funnel control for quadrotors53
Adaptive hybrid Kalman filter for attitude motion parameters estimation of space non-cooperative tumbling target53
Buckling optimization of non-uniformly distributed curved grid-stiffened helicoidal composite panels with cutouts52
Large Eddy Simulation of cavity stabilized ramjet combustion52
Tension-twist coupling morphing wing using a novel mechanical metamaterial52
Design exploration and optimization of aerodynamics and radar cross section for a fighter aircraft52
Prescribed finite-time boundary control of constrained flexible satellite systems with translational motion modeling52
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