王 発明

Wang Faming

  • 特定助教
  • 学位:博士(工学)

基本情報

所属

  • Research Institute of Science and Technology

詳細情報

研究キーワード

  • Numerical analysis
  • Fluid mechanics
  • Detonation
  • Shock wave

研究分野

  • Manufacturing technology (mechanical, electrical/electronic, chemical engineering) Thermal engineering
  • Social infrastructure (civil Engineering, architecture, disaster prevention) Disaster prevention engineering
  • Aerospace, marine, and maritime Engineering Aerospace engineering
  • Manufacturing technology (mechanical, electrical/electronic, chemical engineering) Fluid engineering

論文

Interferometric visualization of detonation waves through premixed detonable jet-train at low mass-flow rate

Elucidation of fuel mixing and consumption states by density field around detonation wave inside a pressure gain combustion channel

Dependence of premixture jet height on detonation wave propagation inside a pressure gain combustion channel

nterferometric visualization of detonation waves inside a pressure gain combustion channel at low-mass flow rates

Visualization of detonation waves inside a rotating-detonation rocket engine by using point-diffraction interferometry

Visualization and CFD of the influence of mixing on detonation wave propagation inside a rotating-detonation engine by using linear detonation channel

講演・口頭発表等

  • Flow Visualization around High-speed Projectile with Point-Diffraction Interferometry
  • Effect of Premixed Jet Height on Propagation of Detonation Wave inside Linear Detonation Channel
  • Numerical and experimental study of actuation characteristics on H2/Air non-premixed rotating detonation engine
  • Flow Visualization around High-speed Projectile with Point-Diffraction Interferometry
  • Numerical Analysis of Propagation of Detonation Wave Plunging Entry the Fuel Jet Train inside Rotating Detonation Combustor
  • Numerical Analysis of the Influence of Mixing on Detonation Wave Propagation inside a Rotating Detonation Engine by using Linear Detonation Channel
  • NUMERICAL ANALYSIS OF THE DETONATION WAVE PROPAGATION IN A LINEARIZED ROTATING DETONATION ENGINE
  • Three-dimensional visualization of shock waves using background-oriented schlieren with light field technique
  • NUMERICAL ANALYSIS OF DETONATION STRUCTURE BY USING CHARIOT
  • Flight Attitude Stabilizing by Side-Jet Generated by Detached Shock Pulsation

所属学会

  • American Institute of Aeronautics and Astronautics

ResearchMapへ移動します

Contact Us

Inquiries about coverage

Public Affairs Division Public Affairs and Communications Department

Tel. 0463-63-4670(direct dialing)