Journal of Aerospace Engineering

Papers
(The TQCC of Journal of Aerospace Engineering is 4. 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 2021-08-01 to 2025-08-01.)
ArticleCitations
Experimental Investigations of Screech Mitigation and Amplification by Beveled and Double-Beveled Nozzles28
Suppression of Low-Reynolds-Number Flow Separation by Controlling the Laminar Separation Bubble with Intermittent Disturbance27
Optimized Design and Analysis of Printed Magnetorquer for a 3-U Nano-Satellite21
Improved Electromechanical Response in Laminated Piezoelectric Plates Using a Zigzag Theory18
Flow Structures around a Square Cylinder: Effect of Corner Chamfering18
Output-Constrained Attitude Tracking Control for Spacecraft with Adaptive Inertia and Disturbance Identifications18
Lift and Tip Vortices Generated by Tapered Backward-Swept and Forward-Swept Wings under Stationary Ground Proximity17
Uniformly Stiffened Cantilever Plates under Bending17
Flow Mechanism of the Shock Structure and Secondary Flow Control in a Supersonic Compressor with a Nonaxisymmetric Endwall16
Design, Modeling, and Ground Test of a Tethered CubeSat with a Rotational Net16
A Compressor Stall Warning System for Aeroengines Based on the Continuous Wavelet Transform and a Vision Transformer16
Experimental and Numerical Research on a Three-Dimensional Inward-Turning Inlet15
An Integrated Tracking Control Approach Based on Reinforcement Learning for a Continuum Robot in Space Capture Missions14
Performance-Based Engineering Framework to Quantify Micrometeoroid Damage to Lunar Surface Structures12
Low-Speed Oblique Impact Response of Adhesively Bonded Dissimilar Single-Lap Joints12
Extended Implicit PIS-ALE Method to Efficient Simulation of Turbulent Flow Domains with Moving Boundaries11
Application of the Improved Incremental Nonlinear Dynamic Inversion in Fixed-Wing UAV Flight Tests11
Satellite Constellation Reconfiguration Using Surrogate-Based Optimization11
Real-Time Data-Driven Inverse Heat Conduction Method for a Reentry Flight Vehicle Based on the Random Forest Algorithm11
Crashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer11
Adaptive Fuzzy Sliding Mode Controller Design Using a High-Gain Observer for a Nonlinear Aeroelastic System under Unsteady Aerodynamics11
Experimental Study on the Durability of China’s Mars Rover’s Mobility System10
Aerodynamic and Flow Characteristics of a Bidirectional S-Shaped Airfoil10
Analytical and Experimental Studies on Modified Wing Configurations of Cessna 172-R Aircraft to Improve Performance10
Numerical Investigation of the Combustion Characteristics of GO2/GCH4 Splash Platelet Injector10
Numerical Study of Flow and Noise Control Mechanism of Shape-Optimized Series Cylinder10
A Simple Numerical Framework for Finite Deflection of Piezoelectric Beams9
Static and Dynamic Characteristics of Nonmetallic Labyrinth Seals Based on Fluid–Solid–Thermal Coupling9
Numerical Investigation of a Pitching NACA 0012 Wing with Plasma-Based Flow Control Using Prediction–Correction Direct-Forcing Immersed Boundary Method9
Control of Shock Oscillations with Successive Ramps in a Hypersonic Inlet–Isolator9
Analysis of the Impact of Tiny Space Debris on Double Satellite Formation for Gravity Recovery Missions9
Rectangular Sonic Jet Control with Supersonic Fluidic Injectors9
Dynamic Crack Propagation along Elastic Interfaces in Double Cantilever Beams under High Loading Rates8
Nonlinear Control of a Novel Class of Tilt-Rotor Quadcopters Using Sliding Mode Method: Theory and Hardware Implementation8
Halo Orbit Maintenance around L1 Point of the Sun-Earth System Using Optimal Control and Lyapunov Stability Theory8
Aerodynamic and Aeroacoustic Optimization of UAV Rotor Based on Proper Orthogonal Decomposition Method8
Investigating Interlaminar Stresses in Stress Concentration Zones of Laminated Composite Shells of Revolution Using Quasi-3D Theory with the Transverse Stress Recovery8
Multiobjective Optimization of Scramjet Strut Geometry Using Computational Fluid Dynamics Approach8
Structure-Actuator Integrated Design of Piezo-Actuated Composite Plate Wing for Active Shape Control8
The Effect of Unsteady Flapping Motion on the Aerodynamic Performance of Bio-Inspired Alula8
Analysis and Optimization of Transmission Performance of Low-Impact Docking Mechanism8
Distributed Finite-Time Attitude Tracking Control for Multiple Rigid Spacecrafts with Full-State Constraints8
Hybrid Modeling Method for the Complex Radiative Cooling Network in the Chinese Space Station8
Additively Manufactured Sound-Absorbing Porous Structures for Airfoil Trailing-Edge Noise Control8
Explicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates8
Honeycomb Parameter-Sensitive Predictive Models for Ballistic Limit of Spacecraft Sandwich Panels Subjected to Hypervelocity Impact at Normal Incidence8
Improved Reinforcement Learning–Based Method for Emergency Mission Planning to Remove Space Debris8
Aerodynamic Parameter Estimation for Near-Stall Maneuver Using Neural Networks and Artificial Bee Colony Algorithm8
Performance Enhancement of Spacecraft Attitude Control Using Modified Robust Design Optimization in Presence of Sensor Noise7
Analysis on Aerodynamic Stability of Blades by an Efficient Fluid–Structure Coupling Method7
A Comparative Study of DWT and EEMD Methods for Validation and Correction of Pyroshock Data7
Fatigue Damage–Based Topology Optimization of Helicopter Tail Rotor Pitch Arm7
Anti-Unwinding Immersion and Invariance Adaptive Attitude Control of Rigid Spacecraft with Inertia Uncertainties7
On the Reductions of Airfoil Broadband Noise through Sinusoidal Trailing-Edge Serrations7
Effect of Rubber Strain Rate on Performance of Aircraft Tire7
Single-Point and Multipoint Design of Propellers for Electric-Powered General Aviation7
Sensitivity-Based Parameterization for Aerodynamic Shape Global Optimization7
Behaviors of Hypersonic Wing under Aerodynamic Heating7
Kinetic Particle Simulations of Plasma and Dust Environments at Robotic Construction Sites near the Lunar Terminator7
Numerical Investigation of Aerodynamic and Aeroheating Characteristics of Blunted Cone and Wedge for High Mach Number Flow7
Source Mechanisms and Control Methods for Aerodynamic Noise7
Electromechanical Deicing of Helicopter Structures with Integrated Ice Detection by Impedance Measurement6
Experimental Investigation of the Flow Characteristics and Noise Generation at the Wing–Wall Junction6
Dynamic Aeroelastic Performance Optimization of Adaptive Aerospace Structures Using Structural Geometric Nonlinearities6
Frequency-Based Adaptive PPF Controller for Vibration Reduction of a Helicopter Shell Body6
Predicting Spatial Distributions of Lighthill’s Aeroacoustic Source Terms Using Steady-State RANS Simulations in Turbocharger Compressors6
Spin Axis Control Using Reaction Wheels: Modeling and Experimental Validation6
Fusion-Based Dual-Task Architecture for Predicting the Remaining Useful Life of an Aeroengine6
A CFD Analysis of the Geometrical Optimization of Slotted Airfoils by Using the RANS k-ω SST Turbulence Model6
Dynamics of Tethered-Coulomb Formation for Debris Deorbiting in Geosynchronous Orbit6
Mechanisms of Hysteresis in the Acceleration and Deceleration Processes of Hypersonic Inlets6
Reviewers6
Coverage Analysis of Remote Sensing Satellites in Concurrent Design Facility6
Machine Learning–Aided Synthetic Air Data System for Commercial Aircraft6
Experimental Investigation of Tip Vortex Formation Noise Produced by Wall-Mounted Finite Airfoils6
Airfoil Self-Noise Reduction by Gradient Distributed Porous Trailing Edges6
Application of Mathematical Modeling to Study Near-Field Pressure Pulsations of a Near-Future Prototype Supersonic Business Aircraft6
Multiobjective Optimization of Double-Wall Cooling Structure of Integrated Strut Flame Stabilizer and Sensitivity Analysis of Parameters6
Structural Health Monitoring and Flight Safety Warning for Aging Transport Aircraft6
Feasibility Study on Handling Lunar Regolith Using Magnetic Force6
Alpha Uncertainty and Disturbance Based Robust Controller for Trajectory Tracking of Octocopter UAV6
Experimental and Numerical Analysis of Pressure-Effect Threat Model Based on SPH Method6
Data-Driven Method for Real-Time Reconstruction of the Structural Displacement Field6
Tuning the Deformation of Flapping Wing to Improve the Flight Efficiency of Dove FWMAV6
Understanding Flow Characteristics in Metal Additive Manufacturing6
Output-Constrained Adaptive Composite Nonsingular Terminal Sliding Mode Attitude Control for a Class of Spacecraft Systems with Mismatched Disturbances and Input Uncertainties6
Experimental Exploration of Bioinspired Planar Wingtip Devices for a Flat-Plate Wing in the Low Reynolds Number Regime6
Optimized Generative Topographic Mapping Method for Aerodynamic Design Optimization6
Investigation of the Dynamic Properties of Viscoelastic Dampers with Three-Chain Micromolecular Configurations and Tube Constraint Effects5
Aerodynamic Optimization and Noise Reduction of a Two-Stage Series Compact Fan5
TD3-Based Model Predictive Control for Satellite Formation-Keeping5
Reviewers5
Research on the Noise Reduction Mechanisms of Bionic Airfoils with Different Serrated Trailing-Edge Structures5
Antinoise Aerodynamic Parameter Estimation Approach for Hypersonic Vehicle Using Dynamic Equation and Flight Data5
Modeling and Adaptive Control Law Design for a Bi-Tiltrotor Unmanned Aerial Vehicle5
Numerical Simulation of the Aerodynamics of a Scaled Free Jet Altitude Test Facility Model5
Research on Dynamic Characteristics Analysis and Control Law Design Method of Model Aircraft in Wind Tunnel–Based Virtual Flight Testing5
A Novel Control Surface for Energy-Optimum Maneuver for Solar-Powered Aircraft5
Experimental Studies on Droplet-Size Distribution in a Reverse-Flow Combustor of a Two-Staged Fuel Injector5
Effect of Perforated Tab on Noise Mitigation of a Mach 1.8 Jet5
Coupled Analysis of Low-Velocity Impact Damage and Compression after Impact Strength of Composite Laminates5
Multiple Model L1 Adaptive Fault-Tolerant Control of Small Unmanned Aerial Vehicles5
Convergence Compensation for Space Contact Semiphysical Simulator Based on Mechanical Structure Dynamics5
Three-Dimensional Composite Approach Angle Constrained Guidance Law with Actuator Lag Consideration5
GPU Implementation and Optimization of a High-Order Spectral Difference Method for Aeroacoustic Problems5
Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip5
Transonic Buffet in Flow Past a Low-Reynolds-Number Airfoil5
Parametric Analysis and Performance Optimization of Landing–Moving Integrated Gear for Mobile Lunar Lander5
Fast Online Trajectory Generation for Time Adjustable Flight Consensus5
Influence of Buffer Substance on Separation Mechanism of CFRP-Based Separation Devices with Shaped Charges5
Uncertainty Quantification and Sensitivity Analysis of Closure Parameters of Transition Models5
A Collaboratively Iterative Sequential Approximate Optimization Method for Aerodynamic Optimization5
Experimental Investigation of Ground Effect on the Vortical Flow Structure of a 40° Swept Delta Wing5
Neural Network–Assisted Initial Orbit Determination Method for Libration Point Orbits5
Natural Frequencies of Soft-Core Composite Sandwich Plates Reinforced by FG Graphene Platelets5
Development of a High-Accuracy Inertia Simulation System for Drive Joints of Space Station Transfer Arm5
Improving Delamination Modeling via Inverse Analysis5
Influence of Structural Flexibility on Nonlinear Vibrations Induced by Orbital Maneuver for a Tethered Spacecraft5
Reviewers5
Unsupervised Fault Detection Driven by Multivariate Time Series for Aeroengines5
Effects of Bioinspired Leading-Edge Tubercles on Flow Separation and Loss in Compressor Cascades with Controlled Diffusion Airfoils4
Suitability of Split Box Direct Tension Testing for Measuring Tensile Strength of Regolith Simulants4
Impact Behaviors of Sandwich Composites Produced by Liquid Resin Infusion: Influences of the Process Parameters4
Specialized Penetrometer Use for Extraterrestrial Surface Characterization4
Identification of Distributed Dynamic Loads in Gradually Varying Two Spatial Dimensions Based on Discrete Cosine Transform and Kalman Filter with Unknown Inputs4
Subcritical Debonding Characterization of GFRP-Concrete Bonded Interface Using Modified Single Cantilever Beam Specimens4
Drag Mitigation of Trilobed Airship Hull through Aerodynamic Comparison with Conventional Single-Lobed Hull4
Hydrodynamic Effects in Wing Fuel Tank Caused by Debris Impact4
A Continuous Nonlinear Sliding Mode Control with Fractional Operators for Quadrotor UAV Systems in the Presence of Disturbances4
Bending Analysis of Sandwich Plates Subjected to Various Mechanical Loadings Using Quasi-Three-Dimensional Theory4
Transition Prediction for Hybrid Laminar Flow Control Flight Test Considering Geometric Uncertainties4
Time-Varying Nonholonomic UAV Formation Control with Trajectory Prediction and Nonlinear Model Predictive Control4
Flight Dynamics Modeling, Trim, Stability, and Controllability of Coaxial Compound Helicopters4
Lamb Wave–Based Structural Health Monitoring for Aluminum Bolted Joints with Multiple-Site Fatigue Damage4
Applications of the Multilayer Porous Medium Modeling Approach for Noise Mitigation4
Retrofitting of an Ultralight Aircraft for Unmanned Flight and Parachute Cargo Drops4
DES of a Slingsby Firefly Aircraft: Unsteady Flow Feature Extraction Using POD and HODMD4
Research on Asteroid Landing with a New Flexible Spacecraft4
Modeling of Biaxial Compression Behavior of Carbon Fiber–Reinforced Composite after Low-Velocity Impact4
Dual Attention Smoothing Adaptation Networks for Aeroengine Multisource Cross-Domain Fault Diagnosis under Category Shift4
Concurrent Subspace Complex Coordination Optimization Method for Structural Layout Synthetical Optimization Problem4
Numerical Analysis of Interface Morphology Effects on Stress Behaviors in Thermal Barrier Coatings with Varied Thicknesses4
Geometrically Exact Aeroelastic Stability Analysis of Composite Helicopter Rotor Blades in Hover by Updated VABS4
Finite-Time Backstepping Attitude Controller for First-Stage Booster Recovery by Parafoil System4
Adaptive Prescribed-Time Tracking Control of Spacecraft with Deferred Full-State Constraints4
Obstacle-Avoidance Safety-Guaranteed Rendezvous Control with a Velocity Safety Corridor and Prescribed Performance4
A 3D-Printing Centered Approach to Mars Habitat Architecture and Fabrication4
Impact Dynamics for Advanced Aerospace Materials and Structures4
Coordinated Control Based on Reinforcement Learning for Dual-Arm Continuum Manipulators in Space Capture Missions4
Trajectory Tracking Control Based on Generalized Rodrigues Parameter for Underactuated VTOL UAVs4
Experimental Study on RP-3 Aviation Fuel Tank Using Oxygen-Consuming Inerting Technology4
Characterization of Nonlinear Birchwood Model with Strain Rate Effect4
Attitude Stability Analysis and Configuration Design of Pyramid Drag Sail for Deorbit Missions4
Finite-Time Guidance and Control for Uncrewed Receiver Aircraft in Aerial Refueling Rendezvous4
Modeling and Contribution Analysis of Vibration Transfer Paths for a Dual-Rotor Aeroengine4
Experimental Investigation of Deployment Process of Large Hoop Truss Antenna for Space4
Entry Guidance with Asymmetric Output Constraints on Drag Acceleration and Predefined-Time Convergence4
Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction4
Adaptive Fault-Tolerant Control Allocation of Flexible Satellite with Infinite-Dimensional Model4
Thermal-Mechanical Coupling Performance and Its Influence on Thermal Stiffness of Cylindrical Roller Bearings4
Development of a Mathematical Model of a Coaxial Compound Helicopter for Trimming and Stability Analysis4
Multilayer Modeling of Delaminated Bilayer Beams and Its Application to Fracture and Buckling Analysis4
Attitude Control Method for Liquid-Filled Flexible Spacecraft Based on Wave-Based Control4
Global Nonlinear Aerodynamic Reduced-Order Modeling and Parameter Estimation by Radial Basis Functions4
Probabilistic-Based Nonlinear Progressive Failure Analysis of Piezoelectric Laminated Composite Shell Panels in Hygrothermal Environment4
Design Method of a Modular Shape-Transition Nozzle for an Axisymmetric Scramjet-Powered Vehicle4
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