Shengji Li

ORCID: 0000-0002-2687-9805
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About
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Research Areas
  • Energetic Materials and Combustion
  • Rocket and propulsion systems research
  • Combustion and Detonation Processes
  • Electrohydrodynamics and Fluid Dynamics
  • Combustion and flame dynamics
  • Geomechanics and Mining Engineering
  • Thermal and Kinetic Analysis
  • Petroleum Processing and Analysis
  • Heat transfer and supercritical fluids
  • Geoscience and Mining Technology
  • Fluid Dynamics and Heat Transfer
  • High-Velocity Impact and Material Behavior
  • Biodiesel Production and Applications
  • Atmospheric aerosols and clouds
  • Laser-induced spectroscopy and plasma
  • Boron and Carbon Nanomaterials Research
  • Hydrogen Storage and Materials
  • Photonic Crystal and Fiber Optics
  • Advanced Combustion Engine Technologies
  • Extraction and Separation Processes
  • Civil and Geotechnical Engineering Research
  • Advanced Fiber Optic Sensors
  • Catalytic Processes in Materials Science
  • Atmospheric chemistry and aerosols
  • Aeolian processes and effects

Hangzhou Dianzi University
2016-2025

Nanjing Tech University
2025

Zhejiang Shuren University
2015

Zhejiang Sci-Tech University
2015

Taiyuan Iron and Steel Group (China)
2014

Taiyuan University of Technology
2014

Zhejiang University
2008

To solve the problems associated with micron-sized aluminum (Al), including sintering, agglomeration, and slag deposition during combustion of aluminized propellants, aluminum–lithium (Al-Li) alloy, prepared by introducing a small amount Li (1.0 wt.%) into Al, was used in place Al. Then, ignition characteristics single Al-Li alloy particles were investigated detail using self-built experimental apparatus multiple characterization methods. The probability, delay time, flame propagation rate,...

10.3390/aerospace10030299 article EN cc-by Aerospace 2023-03-17

Abstract The development of efficient and earth‐abundant water‐splitting electrocatalysts is great importance for energy conversion storage technologies. In this study, surface‐activated amorphous Fe x B catalysts, Fe–B–O@Fe 2 Fe–B–O@FeB , are synthesized remarkable activity the oxygen evolution reaction (OER) achieved, e.g., delivering a current density 10 mA cm −2 at overpotential 260 mV with Tafel slope 57.9 dec −1 OER in alkaline electrolyte. Iron oxide/hydroxide oxidized borate species...

10.1002/admi.201801690 article EN Advanced Materials Interfaces 2019-01-30

Nanosizing and alloying of aluminum (Al) promisingly improve ignition combustion performance Al-based propellants. To aim this, lased-induced characteristics micro/nano-Al aluminum@nickel (Al@Ni) alloy powders at elevated pressures (0.1–3.0 MPa) were investigated the pressure effect on these was correspondingly evaluated. Comparative results demonstrate that nanosizing significantly shorten delay total burn time pressures, with reduction 98.04% 52.28% 1.0 MPa for nano-Al Al@Ni compared to...

10.1016/j.csite.2024.104169 article EN cc-by-nc-nd Case Studies in Thermal Engineering 2024-02-28

It is vital to measure combustion temperature define models accurately. For single fuel particles in powder-fueled ramjets, their size distribution ranges from submicron submillimeter, and burn time short millisecond order. Moreover, the radiation intensity of different types significantly oscillated with several orders magnitude. Current measurement technology facing this challenge. This paper proposes a highly spatiotemporal resolved pyrometry by coupling single-point photomultiplier tube...

10.3390/nano15030223 article EN cc-by Nanomaterials 2025-01-30

Abstract To improve the ignition and combustion performance of aluminum, complementary metal is introduced into it to form binary alloy like Al−Mg, Al−Ti, Al−Zr Al−Li. This paper mainly investigated preparation, characterization, ignition, characteristics Al−Mg powder. Melt atomization technique was used produce spherical powder containing 20 % mass content Mg composition. The crystalline structure, morphology, element distribution, thermal were characterized by XRD, TEM, SEM, EDS, TG‐DSC....

10.1002/prep.202000058 article EN Propellants Explosives Pyrotechnics 2020-08-04

n-Decane-based nanofluid fuels could be one of the most promising alternative as aviation kerosene for aerospace application. However, physical and heat-transfer properties n-decane-based nanofuels have been rarely studied, influence concentration nanoparticles on evaporation characteristics has sparsely investigated. This paper investigated graphite/n-decane emphasized effect adding graphite nanoplatelets (GNPs) these characteristics. It was found that there are a linear increase density...

10.1021/acsomega.1c05343 article EN cc-by-nc-nd ACS Omega 2022-01-17

The mixed aerosols formed by fly ash and ammonium sulfate have a vital impact on the scattering characteristics of atmosphere. This paper proposes to investigate an individual optically levitated aerosol using coupled laser levitation measuring apparatus. were first prepared characterized multiple techniques. results demonstrated that particles completely encapsulated crystals rough porous surface ash, resembling “core-shell” structure. Moreover, columnar exhibit highest regularity when...

10.3390/pr12040769 article EN Processes 2024-04-11

Aluminum/tetrahydrodicyclopentadiene/oleic acid (Al/JP-10/OA) nanofluid fuel is considered a potential for aircraft powered by aviation turbine engines. However, an optimized formula Al/JP-10/OA system inducing secondary atomization and micro-explosion effect improving the burning performance needs to be developed. With this aim, in work, combustion characteristics of pure JP-10, JP-10/OA, JP-10/Al, were experimentally tested, comparative analysis was conducted. Specifically, influence...

10.3390/molecules29081806 article EN cc-by Molecules 2024-04-16

Al-Mg-Li ternary alloy particles can be a promising metal additive to replace aluminum in solid propellants improve combustion efficiency by reducing agglomeration during combustion. In this paper, was prepared and its basic physical chemical characterization parameters were obtained SEM-EDS, ICP-AES, XRD analysis. The ignition characteristics of single under different pressures investigated using self-developed experimental setup. process flame structure significantly affected the...

10.1016/j.csite.2024.104417 article EN cc-by-nc-nd Case Studies in Thermal Engineering 2024-04-18

This paper presents a comparative study on the laser-induced ignition and combustion characteristics between nanometer-sized aluminum (nano-Al) micron-sized (micro-Al) powder stacks. Six different sizes of Al powders (56.0 nm, 74.4 93.4 nm for nano-Al 2.9 μm, 6.1 10.8 μm micro-Al) were selected to conduct experiments, at same operation conditions in static air flow with atmospheric temperature pressure 55% relative humidity. The results demonstrated that delay time is much lower than...

10.1080/00102202.2020.1800659 article EN Combustion Science and Technology 2020-08-06

Abstract This paper presents the experiments and numerical calculations on laser‐induced ignition of single micron‐sized aluminum particle in an atmospheric pressure air flow at low Reynolds number. Experimental results demonstrate that radiation intensity particle, during ignition, experiences first sharp rising, stable equilibrium second steep rising stages. A simplified analytical model was built numerically solved. Numerical show three distinctive stages represent heating, melting...

10.1002/prep.201600215 article EN Propellants Explosives Pyrotechnics 2017-02-20

The n-decane fuel/n-decane-based nanofluid fuel could be one of the most promising alternative fuels as aviation kerosene for aerospace application. This paper proposes Al/n-decane with surfactant sorbitan monooleate (SP-80) and investigates size effect Al nanoparticle (SA, 56.0 nm; SB, 74.4 nm,; SC, 93.4 nm) on its dispersion stability, physical properties, electrostatic breakup performance. Dynamic light scattering (DLS) measurements numerical calculations particle collision demonstrate...

10.1021/acs.energyfuels.9b03332 article EN Energy & Fuels 2019-12-10

Hydrogen peroxide (H2O2) can be considered as a sterilant or green propellant. For common use in industrial application, spray is an effective method to form fine H2O2 droplets. In this paper, electrostatic atomization based on the configuration of needle ring electrodes proposed produce by minimizing its surface tension. The breakup performances ligaments improved increasing electric field intensity, reducing nozzle size, and adjusting suitable volume flow rate. smallest average diameter...

10.3390/mi13050771 article EN cc-by Micromachines 2022-05-13
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