A5020218641- Computational Fluid Dynamics and Aerodynamics
- Combustion and Detonation Processes
- Heat Transfer and Boiling Studies
- Combustion and flame dynamics
- Gas Dynamics and Kinetic Theory
- Plasma and Flow Control in Aerodynamics
- Heat Transfer and Optimization
- Fluid Dynamics and Turbulent Flows
- Rocket and propulsion systems research
- Aerodynamics and Acoustics in Jet Flows
- Electromagnetic Launch and Propulsion Technology
- Fluid Dynamics Simulations and Interactions
- Spacecraft and Cryogenic Technologies
- Fire dynamics and safety research
- Advanced Combustion Engine Technologies
- Risk and Safety Analysis
- Fluid Dynamics and Heat Transfer
- Refrigeration and Air Conditioning Technologies
- Vehicle Routing Optimization Methods
- Energetic Materials and Combustion
- Privacy-Preserving Technologies in Data
- Advanced Photonic Communication Systems
- Spectroscopy and Laser Applications
- Urban and Freight Transport Logistics
- Transportation and Mobility Innovations
Tohoku University
2022-2024
State Key Laboratory of Oil and Gas Reservoir Geology and Exploitation
2024
China University of Mining and Technology
2021-2024
State Key Laboratory of Supramolecular Structure and Materials
2024
Jilin University
2020-2024
Huazhong University of Science and Technology
2022-2024
Wuhan National Laboratory for Optoelectronics
2024
Beihang University
2016-2024
Wuhan University of Science and Technology
2024
Hubei University of Technology
2024
Intelligent Transportation Systems (ITS) utilises the growing trend of both communication technologies and intelligent analytics to make transportation systems more smart efficient. Federated Learning, a privacy-preserving machine learning paradigm shows promise in being applied this field. However, data device heterogeneity, highly dynamic environment ITS pose challenges performance federated learning. One recent approaches address are choose proper participants from available clients...
This paper reports the simultaneous measurements of multiple flow parameters in a scramjet facility operating at nominal Mach number 2.5 using sensing system based on tunable diode-laser absorption spectroscopy (TDLAS). The TDLAS measures velocity, temperature, and water vapor partial pressure three different locations scramjet: inlet, combustion region near flame stabilization cavity, exit combustor. These enable determination variation mode engine, which are critical for evaluating...
Developing an effective strategy to synthesize perfect titanosilicate TS-1 zeolite crystals with desirable morphologies, enriched isolated framework Ti species, and thus enhanced catalytic oxidation properties is a pervasive challenge in crystal engineering. We here used amino acid l-carnitine as growth modifier ethanol cosolvent regulate the morphologies coordination states of zeolites. During hydrothermal crystallization process, introduced can not only tailor anisotropic rates but also...
Abstract Intelligent fault diagnosis in various industrial applications has rapidly evolved due to the recent advancements data-driven techniques. However, scarcity of data and a wide range working conditions pose significant challenges for existing diagnostic algorithms. This study introduces meta-learning method tailored classification motor rolling bearing faults, addressing limited diverse conditions. In this approach, deep residual shrinkage network is employed extract salient features...
Investigations on combustion enhancement and stabilization of liquid kerosene using five different integrated fuel-injection/cavity-based flameholder configurations were conducted in a model combustor cross sections 51 x 70 mm. The entry Mach number wa
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