Engineering
Recursive
100%
Mass Flowrate
100%
Combustor
100%
Isobutane
100%
Design Flow
100%
Computational Fluid Dynamics
100%
Capillary Tube
100%
Suction Line
100%
Performance Prediction
100%
Capacitance
100%
Measurement
100%
Capacitive
100%
Torus
80%
Combustion Chamber
60%
Artificial Neural Network Model
50%
Coupling Effect
50%
Rate Range
50%
Inlet Pressure
50%
Homogeneous Model
50%
Computational Complexity
50%
Saturation Pressure
50%
Mutual Capacitance
50%
Flue Gas
40%
Flame
40%
Prototype
20%
Fuel
20%
Outlet Pipe
20%
Simulation Result
20%
Cross Section
20%
Burnt Gas
20%
Reactant
20%
Momentum Flux
20%
Combines
20%
Good Agreement
20%
Data Point
20%
Recirculation
20%
Flow Pattern
20%
Design Iteration
20%
Development
20%
Flow Dynamics
20%
Progress Bar
16%