2023年11期
刊物介紹
“Plasma Science & Technology”（等離子體科學(xué)和技術(shù)）是中國科學(xué)院等離子體物理研究所主辦的英文版學(xué)術(shù)期刊。其宗旨是向國內(nèi)外報導(dǎo)我國等離子體科學(xué)界和國外科學(xué)家在高溫等離子體、低溫等離子體、天體空間等離子體、放電等離子體和激光等離子體等各個領(lǐng)域在基礎(chǔ)研究、實驗探索、裝置建設(shè)和應(yīng)用開發(fā)中所取得的具有新意的學(xué)術(shù)成果或階段性成果，并刊登反映這些學(xué)科國際、國內(nèi)發(fā)展新方向、新動態(tài)的綜述，以及與等離子體有關(guān)的交叉學(xué)科和應(yīng)用方面的最新成就等。
Plasma Science and Technology
SPECIAL ISSUE ARTICLES
- Wet flashover voltage improvement of the ceramics with dielectric barrier discharge
- Experimental and numerical investigation on the uniformity of nanosecond pulsed dielectric barrier discharge influenced by pulse parameters
- Preparation of highly efficient antibacterial non-woven by facile plasma-induced graft polymerizing of DADMAC
- Multiple chemical warfare agent simulant decontamination by self-driven microplasma
PAPERS
- High-order field theory and a weak Euler-Lagrange-Barut equation for classical relativistic particle-field systems
- Investigation of phase modulation and propagation-route effect from unmatched large-scale structures for Doppler reflectometry measurement through 2D full-wave modeling
- SOLPS-ITER drift modeling of neon impurity seeded plasmas in EAST with favorable and unfavorable toroidal magnetic field direction
- Preparation of a beam emission spectroscopy diagnostic based on a Lymanalpha line to diagnose core and edge-plasma density fluctuation on the HL-2A tokamak
- Development of an atmospheric fluorocarbon plasma jet generated by pulse modulated microwave discharge
- Ionization wave propagation and cathode sheath formation due to surface dielectricbarrier discharge sustained in pulsed mode
- Research on degradation mechanism of trichlorobenzene and Hg0 by nonthermal plasma catalysis
- Non-invasive optical characterization and estimation of Zn porosity in gas tungsten arc welding of Fe-Al joints using CR model and OES measurements
- Design of new resonant magnetic perturbation coils on the J-TEXT tokamak
- A study of grid failure mode drivers and methods for accelerated life testing of a 30cm diameter ion thruster