Junqiang Bai
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View article: Spatial dependencies and long-run dynamics of the Environmental Kuznets Curve in West Africa: an analysis of growth vs. emissions
Spatial dependencies and long-run dynamics of the Environmental Kuznets Curve in West Africa: an analysis of growth vs. emissions Open
Validating the Environmental Kuznets Curve (EKC) hypothesis has been a core subject for decades. Still, its universality is contested in contemporary studies due to prior region-specific outcomes. Comprehensively estimating its applicabili…
View article: Correlating Cross-Iteration Noise for DP-SGD using Model Curvature
Correlating Cross-Iteration Noise for DP-SGD using Model Curvature Open
Differentially private stochastic gradient descent (DP-SGD) offers the promise of training deep learning models while mitigating many privacy risks. However, there is currently a large accuracy gap between DP-SGD and normal SGD training. T…
View article: Towards Better Optimization For Listwise Preference in Diffusion Models
Towards Better Optimization For Listwise Preference in Diffusion Models Open
Reinforcement learning from human feedback (RLHF) has proven effectiveness for aligning text-to-image (T2I) diffusion models with human preferences. Although Direct Preference Optimization (DPO) is widely adopted for its computational effi…
View article: FlowerTune: A Cross-Domain Benchmark for Federated Fine-Tuning of Large Language Models
FlowerTune: A Cross-Domain Benchmark for Federated Fine-Tuning of Large Language Models Open
Large Language Models (LLMs) have achieved state-of-the-art results across diverse domains, yet their development remains reliant on vast amounts of publicly available data, raising concerns about data scarcity and the lack of access to do…
View article: Nonlinear aeroelastics of a three-degree-of-freedom airfoil with control surface hysteresis stiffness in a dynamic stall flow
Nonlinear aeroelastics of a three-degree-of-freedom airfoil with control surface hysteresis stiffness in a dynamic stall flow Open
View article: Static Segmentation by Tracking: A Frustratingly Label-Efficient Approach to Fine-Grained Segmentation
Static Segmentation by Tracking: A Frustratingly Label-Efficient Approach to Fine-Grained Segmentation Open
We study image segmentation in the biological domain, particularly trait and part segmentation from specimen images (e.g., butterfly wing stripes or beetle body parts). This is a crucial, fine-grained task that aids in understanding the bi…
View article: Aerodynamic performance analysis of different damaged types of a turboprop wing
Aerodynamic performance analysis of different damaged types of a turboprop wing Open
Wingtiploss and bullet impact are potential hazards faced by existing transport aircraft, posing a serious threat to flight safety. These damages create asymmetric rolling moments that lead to aircraft instability and aerodynamic degradati…
View article: Pore‐Throat Differences Across Flow Units in Low‐Permeability Sandstone Reservoirs: Impact on Movable Fluid Saturation in the Triassic Chang 6 Reservoir, Jiyuan Oilfield, Ordos Basin, China
Pore‐Throat Differences Across Flow Units in Low‐Permeability Sandstone Reservoirs: Impact on Movable Fluid Saturation in the Triassic Chang 6 Reservoir, Jiyuan Oilfield, Ordos Basin, China Open
Low‐permeability sandstone reservoirs, as a subset of unconventional oil and gas reservoirs, have gained significant attention due to their distinct exploration and development potential. These reservoirs exhibit intricate heterogeneity, v…
View article: Improved Aerodynamic-Propulsion Integration Model for Distributed-Electric-Propulsion System and its Integration in Sizing for Hybrid-Electric Distributed-Propulsion Aircraft
Improved Aerodynamic-Propulsion Integration Model for Distributed-Electric-Propulsion System and its Integration in Sizing for Hybrid-Electric Distributed-Propulsion Aircraft Open
View article: Improved Model for Hydrogen Fuel Cell System Design and its Integration in Sizing for Hybrid-Electric-Propulsion Aircraft
Improved Model for Hydrogen Fuel Cell System Design and its Integration in Sizing for Hybrid-Electric-Propulsion Aircraft Open
View article: Investigation Of An Extended Single Particle Model Incorporating Electrolyte Kinetics, Temperature Effects, and Side Reactions for Improved Battery Performance Simulation Under High Charge/Discharge Rates and Low-Temperature
Investigation Of An Extended Single Particle Model Incorporating Electrolyte Kinetics, Temperature Effects, and Side Reactions for Improved Battery Performance Simulation Under High Charge/Discharge Rates and Low-Temperature Open
View article: Quasi-three-dimensional high-lift wing design approach considering three-dimensional effects of slipstream for distributed electric propulsion aircraft
Quasi-three-dimensional high-lift wing design approach considering three-dimensional effects of slipstream for distributed electric propulsion aircraft Open
The efficient utilization of propeller slipstream energy is important for improving the ultra-short takeoff and landing capability of Distributed Electric Propulsion (DEP) aircraft. This paper presents a quasi-three-dimensional (2.5D) high…
View article: Data-driven surrogate model for aerodynamic design using separable shape tensor method
Data-driven surrogate model for aerodynamic design using separable shape tensor method Open
In the context of increasing dimensionality of design variables and the complexity of constraints, the efficacy of Surrogate-Based Optimization (SBO) is limited. The traditional linear and nonlinear dimensionality reduction algorithms are …
View article: Parameter effect on the novel swashplateless rotor control
Parameter effect on the novel swashplateless rotor control Open
To achieve underactuated control, a novel swashplateless rotor configuration of asymmetric inclined hinges which can be driven by periodic sinusoidal torque is studied, hopefully eliminating the conventional swashplate mechanism and multip…
View article: A Novel Aerodynamic Performance Prediction Method Considering Viscous Effect for Ducted Fan-Wing Coupling Configuration
A Novel Aerodynamic Performance Prediction Method Considering Viscous Effect for Ducted Fan-Wing Coupling Configuration Open
View article: Trajectory Planning and Control Design for Aerial Autonomous Recovery of a Quadrotor
Trajectory Planning and Control Design for Aerial Autonomous Recovery of a Quadrotor Open
One of the most essential approaches to expanding the capabilities of autonomous systems is through collaborative operation. A separated lift and thrust vertical takeoff and landing mother unmanned aerial vehicle (UAV) and a quadrotor chil…
View article: Effects of Static Stability Margin on Aerodynamic Design Optimization of Truss-Braced Wing Aircraft
Effects of Static Stability Margin on Aerodynamic Design Optimization of Truss-Braced Wing Aircraft Open
Currently, the aviation industry is facing an oil and energy crisis and is contributing much more greenhouse gas emissions to the environment. Aircraft design approaches, such as aerodynamic shape optimization, new configuration concepts, …
View article: Performance analysis and flow mechanism of channel wing considering propeller slipstream
Performance analysis and flow mechanism of channel wing considering propeller slipstream Open
The development of the Urban Air Mobility concept has proposed stringent requirements for the fixed-wing vehicle's Short/Vertical Take-Off and Landing (S/VTOL) performance. With its lift-enhancing impact, the channel wing, can improve airc…
View article: Aerodynamic Optimization Design of Supersonic Wing Based on Discrete Adjoint
Aerodynamic Optimization Design of Supersonic Wing Based on Discrete Adjoint Open
Reducing fuel consumption and improving the economy by effectively reducing cruising drag is the main objective of the aerodynamic design of supersonic civil aircraft. In this paper, the aerodynamic optimization design system based on the …
View article: Multi-point aero-structural design optimization of wings considering drag-divergence constraints
Multi-point aero-structural design optimization of wings considering drag-divergence constraints Open
Considering the drag-divergence performance as a constraint, this paper presents a multi-point aero-structural design optimization of wings on a wing-body-tail-engine configuration of long-range dual-aisle civil aircraft by using a gradien…
View article: Adjoint-based robust optimization design of laminar flow wing under flight condition uncertainties
Adjoint-based robust optimization design of laminar flow wing under flight condition uncertainties Open
It is an inherent uncertainty problem that the application of laminar flow technology to the wing of large passenger aircraft is affected by flight conditions. In order to seek a more robust natural laminar flow control effect, it is neces…
View article: Study on design characteristics of airfoil pressure distribution for low Mach number general aircraft
Study on design characteristics of airfoil pressure distribution for low Mach number general aircraft Open
This paper studies several problems that may exist in the aerodynamic design of low Mach number general aircraft, and discusses the design characteristics of the pressure distribution of some related airfoils while part of the characterist…
View article: Fluid mechanism analysis on the interaction between natural laminar flow nacelle and wingbody on a transonic aircraft
Fluid mechanism analysis on the interaction between natural laminar flow nacelle and wingbody on a transonic aircraft Open
A transonic natural laminar flow (NLF) nacelle, which is a streamlined fairing used to contain a turbofan engine and mounted under the wing of civil aircraft, can reduce friction drag. Because the fluid mechanism of the interaction between…
View article: Electrical Characteristics of Photovoltaic Cell in Solar-Powered Aircraft During Cruise
Electrical Characteristics of Photovoltaic Cell in Solar-Powered Aircraft During Cruise Open
Aiming to study the electrical characteristics of photovoltaic cells during the flight of solar-powered unmanned aerial vehicles, this work combines a photovoltaic cell equivalent circuit model and a thermodynamic model. The influence of w…
View article: Impact Response Prediction Method of Packaging Systems with a Key Component considering Different Excitations and Cushioning Materials
Impact Response Prediction Method of Packaging Systems with a Key Component considering Different Excitations and Cushioning Materials Open
Nonlinear dynamic models of the packaging systems that consider different excitations and cushioning materials are proposed to analyze their impact responses in this paper. To solve the nonlinear dynamic equations of the models, Newmark me…
View article: A Nonlinear Model and Parameter Identification Method for Rubber Isolators under Shock Excitation in Underwater Vehicles
A Nonlinear Model and Parameter Identification Method for Rubber Isolators under Shock Excitation in Underwater Vehicles Open
Rubber isolators are usually used to protect high-precision equipment of autonomous underwater vehicles (AUVs), avoiding damage from overlarge dynamic excitation. Considering the nonlinear properties of the rubber material, the nonlinear b…
View article: A Review of Riemann Solvers for Hypersonic Flows
A Review of Riemann Solvers for Hypersonic Flows Open
View article: Exploration of high-altitude dynamic soaring based on six-degree-of-freedom model
Exploration of high-altitude dynamic soaring based on six-degree-of-freedom model Open
Dynamic soaring is an emerging flight range-extension technology that effectively reduces UAV's energy consumption by deriving wind energy from lateral gradient wind fields. Comparing with the small UAV's near the surface, the application …
View article: Multi-object aerodynamic design optimization using deep reinforcement learning
Multi-object aerodynamic design optimization using deep reinforcement learning Open
Aerodynamic design optimization is a key aspect in aircraft design. The further evolution of advanced aircraft derivatives requires a powerful optimization toolbox. Reinforcement learning (RL) is a powerful optimization tool but has rarely…
View article: Radar Cross Section Reduction and Shape Optimization using Adjoint Method and Automatic Differentiation
Radar Cross Section Reduction and Shape Optimization using Adjoint Method and Automatic Differentiation Open
An efficient Radar Cross Section (RCS) gradient evaluation method based on the adjoint method is presented. The Method of Moments is employed to solve the Combined Field Integral Equation (CFIE) and the corresponding derivatives computing …