Menglei Li

ORCID: 0009-0006-9347-058X
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About
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Research Areas
  • Rocket and propulsion systems research
  • Advanced Combustion Engine Technologies
  • Computational Fluid Dynamics and Aerodynamics
  • Heat transfer and supercritical fluids
  • Combustion and flame dynamics
  • Combustion and Detonation Processes
  • Carbon dioxide utilization in catalysis
  • Gas Dynamics and Kinetic Theory
  • CO2 Reduction Techniques and Catalysts
  • Plasma and Flow Control in Aerodynamics
  • Thermography and Photoacoustic Techniques
  • Integrated Energy Systems Optimization
  • Aerodynamics and Acoustics in Jet Flows
  • Advanced X-ray and CT Imaging
  • Smart Grid and Power Systems
  • Power Systems and Renewable Energy
  • High-Voltage Power Transmission Systems
  • Catalysis for Biomass Conversion
  • Thermodynamic properties of mixtures
  • Energy Load and Power Forecasting
  • Microbial Metabolic Engineering and Bioproduction
  • Industrial Vision Systems and Defect Detection
  • Chemical Thermodynamics and Molecular Structure
  • Electrohydrodynamics and Fluid Dynamics
  • Biochemical and biochemical processes

National University of Defense Technology
2022-2025

Huazhong University of Science and Technology
2022-2023

Nanjing Institute of Technology
2023

Qilu University of Technology
2023

Shandong Academy of Sciences
2023

Weifang University
2020

East China Normal University
2010

Investigating the throttling characteristics of Rocket-Based Combined Cycle (RBCC) engines in ejector mode is crucial for adapting to varied flight mission demands. This study employs validated RANS numerical methods investigate effects on an experimental kerosene-fueled RBCC engine under two representative conditions: ground take-off (Mach 0) and supersonic 2.0). Results indicate that, at Mach 0, reduces entrained secondary stream increases mixing efficiency, but exacerbates losses, which...

10.1016/j.csite.2024.104150 article EN cc-by-nc Case Studies in Thermal Engineering 2024-02-20

Flame stabilization characteristics in the supersonic combustor with a circular cross-section strut were experimentally investigated. The Mach number, stagnation pressure, and temperature of inflow 2.52, 1.60 MPa, 1486 K, respectively. Compared to wedge-shaped recirculation flow at base rectangular strut, conical possessed more favorable geometry characterized by longer length, larger volume, small surface. When fueled hydrogen, equipped both could achieve self-sustaining combustion. In...

10.1063/5.0186980 article EN Physics of Fluids 2024-01-01

The supersonic combustor with an annular cross section has the potential to enhance fuel/air mixing because height of flow path is relatively low. However, efforts that have been dedicated this topic are exiguous. In study, numerical simulations were conducted reveal process in paths. Mach number, total temperature, and pressure entrance 2.35, 300 K, 101.325 kPa, respectively. (H) varied from 7.5 12.5 mm, but equivalent diameter was 37.74 mm for all cases. cases a jet orifice number (Nj) 8,...

10.1063/5.0245094 article EN Physics of Fluids 2025-02-01

Nucleoside analogs are commonly used drugs for the treatment of cancer and viral infections. deoxyribosyltransferase (NDT) is one key enzymes required biosynthesis deoxynucleotides. The feasibility biochemical transformation processes usually greatly dependent on cost biocatalysts. Therefore, immobilizing reusing biocatalysts an approach to be considered bring biotransformations closer industrial feasibility, since it not only allows reused but can also improve their stability under several...

10.20944/preprints202403.0795.v1 preprint EN 2024-03-13

To reduce the drag generated by recirculation flow at rocket base in a Rocket-Based Combined Cycle (RBCC) engine operating ramjet/scramjet mode, novel annular RBCC based on central plug cone was proposed. The performance loss mechanism caused and influence of configuration thrust were studied. Results indicated that extended through entire combustor, which creates an extensive range "low-kinetic-energy zone" center leads to loss. serving as surface structure had restrictive effect internal...

10.1016/j.cja.2023.11.021 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2023-12-01

As a potential alternative to fossil-based fuels, cellulosic ethanol has attracted much attention due its great benefit energy sustainability and environmental friendliness. However, at present, the industrial competitiveness of production is still insufficient compared with fuels because higher costs. Expanding range lignocellulosic biomass may be promising measure promote economical ethanol. Corn fiber, byproduct from corn deep-processing, an attractive feedstock for rich carbohydrate...

10.3390/fermentation9080743 article EN cc-by Fermentation 2023-08-09

The Rocket-Based Combined-Cycle (RBCC) engine integrates the preponderance of ramjet and rocket engines. It can perform excellently at a lower Mach number than while consuming less fuel rocket. higher specific impulse under flight conditions guarantees competitiveness application prospect an RBCC for reusable space transportation hypersonic cruise vehicles. With wide range numbers, flow choking between primary secondary streams in inner passage becomes complicated. not only affects mass...

10.1063/5.0145047 article EN cc-by AIP Advances 2023-08-01

The ejector mode of the Rocket-Based Combined-Cycle (RBCC) engine is characterized by high fuel consumption. This study aimed at investigating influence rocket fuel-rich degree on RBCC engine’s performance under combined with simultaneous mixing and combustion (SMC). Numerical simulations were conducted for various ratios ( <a:math xmlns:a="http://www.w3.org/1998/Math/MathML" id="M1"><a:mi>Φ</a:mi><a:mo>=</a:mo><a:mn>1.6</a:mn><a:mo>~</a:mo><a:mn>3.2</a:mn></a:math> ) subsonic <c:math...

10.1155/2024/4340688 article EN cc-by International Journal of Aerospace Engineering 2024-02-06

Impinging-jet injectors, liquid–liquid coaxial swirl and pintle injectors are representative in liquid rocket engines (LRE). For these the atomization processes all involve impingement, including jet–jet, sheet–sheet, jets/sheet–sheet respectively. After a sheet forms fragments. Based on similarities, reviewing published literature spray characteristics of three LRE is necessary will facilitate investigation to meet progress variable-thrust LRE. This review covers following aspects...

10.1063/5.0223894 article EN Physics of Fluids 2024-09-01

The recent several decades have witnessed more and three-dimensional (3D) intersections in urban traffic infrastructure. Therefore, modeling road network 3D space becomes an essential step study, visualization, micro-simulation, etc. Unlike planar which roads could be simply represented by their centerlines, a line-based model tends to mislead readers, while representing with surfaces might overcome this drawback certain degree. surface built based on centerlines. However, existing...

10.1109/iccet.2010.5485244 article EN 2010-01-01

With the continuous increase in capacity of renewable energy generation our country, effectively balancing supply and demand contradictions power system has become a significant challenge for load regulation system. In response to this issue, paper proposes method plant auxiliary participation peak shaving grid. By establishing analyzing incentive mechanism model contribution loads shaving, an electricity pricing strategy is formulated based on model. This utilizes real grid data validate...

10.1109/ic2ecs60824.2023.10493785 article EN 2023-12-29

RBCC engines can operate efficiently in a wide fight range, which is promising for the propulsion system of space transportation and supersonic cruise aircraft. During mode transition engines, parameters vary considerably. Particularly, ejector-to-ramjet transition, matching requirements between inlet combustor engine are improved. And integration embedded rocket introduces many new characteristics to flow field inlet. The during numerically studied, result shows that impact jet makes...

10.1109/icmae56000.2022.9852897 article EN 2022-07-20
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