Keyphrases
Non-premixed
80%
Jet Diffusion Flame
67%
Jet Flame
52%
Flame Lift-off
52%
Plasma Discharge
48%
Pulsed Jet
48%
Reynolds number
34%
Ignition
34%
Puffing
33%
Tribrachial Flame
32%
Plasma-activated Water
32%
Reattachment
32%
Bluff Body
32%
Plasma Actuator
32%
Non-premixed Flame
32%
Nozzle
30%
Hydrogen Peroxide
30%
Flame Stabilization
29%
Vortex Ring
29%
Coflow
29%
Flame Structure
27%
Laminar Flame Speed
26%
Co-flow Jet
26%
Flame Displacement Speed
24%
Celerity
24%
Lift-off
24%
Flame Propagation
22%
Nitrite
21%
Flame Spread Rate
21%
Nitrate
21%
Combustion
20%
Low Reynolds number
20%
Injection Condition
19%
Annular Plasma
18%
Plasma-assisted Combustion
16%
Optimal Energy Management
16%
Laser-induced Fluorescence Imaging
16%
OH Planar Laser Induced Fluorescence
16%
Reciprocating piston
16%
Turbulent Structure
16%
Turbulent Dynamics
16%
Thrust Vectoring
16%
Secondary Injection
16%
Plasma Technology
16%
Turbulent Jet Flame
16%
Rose Window
16%
Flat Flame
16%
Fuel Activation
16%
Plasma Energy
16%
Plasma-activated
16%
Engineering
Flames
100%
Diffusion Flame
75%
Electric Field
58%
Reattachment
57%
Dielectrics
49%
Actuator
48%
Reynolds' Number
46%
Ignition
34%
Flow Velocity
32%
Combustor
32%
Propagation Speed
32%
Premixed Flame
32%
Vortex
30%
Flame Propagation
28%
Air Flow
25%
Injection Velocity
24%
Methane
20%
Nozzle Exit
18%
Fuel Injection
17%
Corona Discharge
16%
Planar Laser-Induced Fluorescence
16%
Pressure Drop
16%
Laser-Induced Fluorescence Imaging
16%
Reciprocating Piston
16%
Injection Time
16%
Thrust Angle
16%
Flame Stability
16%
Reference Fuel
16%
Dielectric Fluid
16%
Condensation Heat Transfer
16%
Microchannel
16%
Efficiency Coefficient
16%
Catalyst Bed
16%
Fluid Viscosity
16%
Reaction Zone
16%
Injection Pressure
16%
Conservation Equation
16%
Convergent
16%
Parametric Study
16%
Finite Volume Method
16%
Pressure Ratio
16%
Nozzle Pressure
16%
Theoretical Value
16%
Propulsion System
16%
Ambient Pressure
16%
Hydrodynamics
16%
Energy Management
16%
Reinforcement Learning
16%
Learning Control
16%
Gas Mixture
16%
