Journal of Aerospace Engineering
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EISSN:1943-5525|ISSN:0893-1321|Disc:The Journal of Aerospace Engineering promotes the implementation and development of space and aerospace technologies and their transfer to other civil engineering applications. Topics of interest include aerodynamics, computational fluid dynamics, wind tunnel testing of buildings and structures, aerospace structures and materials, advanced composite materials, dynamics and control, real-time data acquisition, space engineering and construction, lunar base construction, field and remote sensing, and robotics|Priority:6|Publisher:American Society of Civil Engineers|
Recent Submissions
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Improving Performance of Ensemble Prediction Models for Mach Number in Wind Tunnels Using Metalearning
(ASCE, 2024/05/01)Accurate prediction of Mach numbers is of paramount importance in wind tunnel experiments. While ensemble prediction models have shown promising performance compared with single-model approaches, existing ensemble methods ... -
GPU Implementation and Optimization of a High-Order Spectral Difference Method for Aeroacoustic Problems
(ASCE, 2024/05/01)This study focuses on the implementation of the spectral difference (SD) method on hexahedral elements to NVIDIA graphics processing units (GPUs) using the Compute Unified Device Architecture (CUDA) for aeroacoustic problems. ... -
Distributed Finite-Time Attitude Tracking Control for Multiple Rigid Spacecrafts with Full-State Constraints
(ASCE, 2024/05/01)This paper studies the distributed attitude tracking control problem for rigid spacecraft under a directed graph with external disturbances and full-state constraints. First, because only a subset of the follower spacecraft ... -
Experimental Study of the Vibration of Blades Induced by Flow and Sound in a Plane Cascade under Low Wind Speed
(ASCE, 2024/07/01)Vibration causes compressor rotor blade failure that affects aeroengine safety. Therefore, a plane cascade model of rotor blades was developed to capture the vibration phenomenon. The blade vibration, vortex shedding, and ... -
Multilayer Modeling of Delaminated Bilayer Beams and Its Application to Fracture and Buckling Analysis
(ASCE, 2024/05/01)A new beam element only having the translational displacement degrees of freedom is developed to analyze fracture and buckling behaviors of bilayer beams or columns with delamination using the multilayer modeling method. ... -
Multiscale Numerical Modeling of 2D C/C Composites Considering Pore Size Distribution
(ASCE, 2024/07/01)This study proposes a multiscale numerical modeling procedure to evaluate the elastic properties of two-dimensional (2D) eight-harness satin woven carbon/carbon (C/C) composites. The multiscale modeling technique consists ... -
Rub-Impact Dynamics of Offset Disc Rotor with Imbalance and Loosening Pedestal
(ASCE, 2024/05/01)It is easy for rotating machinery to produce looseness at the pedestal after long-term operation. The looseness of the pedestal causes the sudden increase of the vibration for the rotor, which leads to the rub-impact between ... -
Development of a High-Accuracy Inertia Simulation System for Drive Joints of Space Station Transfer Arm
(ASCE, 2024/05/01)With a focus on crewed spaceflight and space station construction, this research developed a high-accuracy inertia simulation system for the drive joints of the space station transfer arm. To achieve this objective, both ... -
Time-Varying Nonholonomic UAV Formation Control with Trajectory Prediction and Nonlinear Model Predictive Control
(ASCE, 2024/05/01)This paper proposes a time-varying unmanned aerial vehicle (UAV) formation control method based on trajectory prediction and nonlinear model predictive control (NMPC). First, in formation control, the nominal controller ... -
Drag Reduction Mechanism of Array Microslit-Opposed Jets in the Passivation Leading Edge of High-Speed Aircrafts
(ASCE, 2024/07/01)In order to meet the demanding drag reduction requirements of high-speed aircraft, the drag reduction mechanism of array microslit-opposed jets in the passivation leading edge is studied using a numerical method based on ... -
Evolution Characteristics Analysis of Supersonic Inlet Buzz with High-Order Dynamic Mode Decomposition Method
(ASCE, 2024/05/01)The buzz evolution process of an axisymmetric supersonic inlet was investigated numerically and analyzed using the high-order dynamic mode decomposition (HODMD) method. Driven by an increasing back-pressure, the flow field ... -
A Force- and Position-Based Distortion Compensation Method for a Hardware-in-the-Loop Simulator of Space Docking
(ASCE, 2024/05/01)Hardware-in-the-loop simulation is an important way to test the complex contact process of two spacecraft docking in space. Hardware-in-the-loop simulations are known to be unstable and divergent because of various unexpected ... -
Research on Oscillation Response of Pressure-Combustion-Thrust System in Solid Rocket Motor
(ASCE, 2024/07/01)In order to study the combustion instability of solid rocket motors, the vibration-acoustic vibration-burning rate oscillation-thrust oscillation coupling system of solid rocket motors is analyzed. In this paper, a numerical ... -
Data-Driven Method for Real-Time Reconstruction of the Structural Displacement Field
(ASCE, 2024/05/01)Accurate real-time displacement field reconstruction based on limited measurement points is crucial for spacecraft on-orbit monitoring. This study proposes a data-driven displacement field reconstruction method called ... -
An Enhanced Global–Local Higher-Order Model for Thermal Expansion Analysis of Laminated Panels Reinforced by Carbon Nanotubes
(ASCE, 2024/07/01)Carbon nanotubes (CNTs) are added to the matrix according to proper distribution configurations by many researchers to improve the stiffness of laminated composites. However, the distribution configurations of CNTs may ... -
Finite-Time Backstepping Attitude Controller for First-Stage Booster Recovery by Parafoil System
(ASCE, 2024/01/01)Controllable parafoil is one of the most important means to fulfill the recovery of first-stage booster of a rocket due to its high reliability and low cost. However, as a lightweight flexible aircraft, the parafoil and ... -
Low-Thrust Station-Keeping Strategy toward Exploiting the Resonances in the Geostationary Region
(ASCE, 2024/03/01)Low-thrust propulsion systems are widely used in space missions due to their high specific impulse and reduced propellant consumption. However, current research focuses on eliminating drifts in low-thrust maneuvers, resulting ... -
Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip
(ASCE, 2024/05/01)The use of flared folding wingtip (FFWT) for load alleviation has been considered in recent studies. Most studies analyzed FFWT based on the linear assumption and ignored the nonlinearity of large wingtip folding angle. ... -
Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction
(ASCE, 2024/03/01)Sandwich panels have attracted widespread attention owing to their lightweight and ability to meet strength, energy absorption, and thermal resistance requirements. Therefore, they are useful in the automotive, aerospace, ... -
Nonlinear Stability of Curved Multiphase Composite Panels: Influence of Agglomeration in Randomly Distributed Carbon Nanotubes with Nonuniform In-Plane Loads
(ASCE, 2024/05/01)The nonlinear stability characteristics of doubly curved panels made of three-phase composites with randomly dispersed carbon nanotubes [randomly dispersed carbon nanotube reinforced fiber composites (RD-CNTRFC)] subjected ...