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Keyphrases
Combustion
100%
Burning Rate
73%
Oxidizer
69%
Solid Fuel
65%
Nano-aluminum
62%
Propellant
59%
Equivalence Ratio
58%
Regression Rate
49%
Diffusion Flame
45%
Ignition Delay Time
44%
Aluminum Particles
43%
Hybrid Rocket Motor
38%
Ignition
37%
Oxygen Diffusion
36%
Methane-oxygen
36%
Particle Size
34%
Hydroxyl-terminated Polybutadiene
32%
Combustion Efficiency
30%
Hydrogen Peroxide
29%
Hybrid Rocket
29%
Deflagration
29%
Combustion Behavior
28%
Red Fuming Nitric Acid
27%
Flame Stability
25%
Burner
24%
Chamber Pressure
23%
Liquid Water
23%
Flame Propagation
22%
Propulsion System
19%
High Pressure
19%
Impingement Angle
19%
Flame Speed
18%
Solid Propellant
18%
Boron
18%
Reynolds number
18%
Premixed Methane
18%
Non-premixed
18%
Flow Area
18%
Water Mixtures
18%
Linear Burning Rate
18%
Micron-sized Aluminum
17%
Priming Event
16%
Mass Burning Rate
16%
Pressure Range
15%
Gaseous Oxygen
15%
Peak Pressure
15%
Hydrocarbon Fuel
15%
Low Pressure
15%
Injector
15%
Pressure Dependence
15%
Engineering
Aluminum
86%
Burning Rate
80%
Ignition
63%
Oxidizer
59%
Reactant
58%
Equivalence Ratio
54%
Diffusion Flame
47%
Solid Fuel
45%
Rocket Engine
44%
Methane
40%
Ignition Delay
40%
Hydrogen
31%
Jet
28%
Nitric Acid
27%
Flame Stability
25%
Propulsion System
24%
Delay Time
22%
Chamber Pressure
21%
Peak Pressure
21%
Flow Velocity
20%
Deflagration
19%
Strand
19%
Experimental Investigation
18%
Reynolds' Number
18%
Flow Area
18%
Flame Propagation
17%
Mass Flowrate
17%
Pressure Level
16%
Primary Flow
16%
Hybrid Rocket Engine
15%
Initial Temperature
15%
Pressure Range
15%
Flow Rate
14%
Combustion Chamber
13%
Secondary Flow
13%
Size of Particle
12%
Internal Diameter
11%
Nitrogen
11%
Ammonium
11%
Pyrolysis
11%
Dust Cloud
11%
Fossil Fuel
10%
Cold Flow
10%
Experimental Result
10%
Air Mixture
10%
Premixed Flame
9%
Numerical Model
9%
Nanoscale
9%
Gas-Phase
9%
Nanoparticle
9%
