Keyphrases
Combustion
94%
Oxidizer
66%
Equivalence Ratio
61%
Solid Fuel
61%
Burning Rate
61%
Propellant
51%
Aluminum Particles
47%
Nano-aluminum
46%
Regression Rate
43%
Diffusion Flame
42%
Ignition Delay Time
41%
Oxygen Diffusion
35%
Methane-oxygen
35%
Ignition
35%
Hybrid Rocket
33%
Hybrid Rocket Motor
32%
Combustion Efficiency
32%
Hydrogen Peroxide
29%
Particle Size
28%
Hydroxyl-terminated Polybutadiene
28%
Deflagration
26%
Chamber Pressure
26%
Red Fuming Nitric Acid
25%
Propulsion System
25%
Burner
25%
Flame Propagation
24%
Flame Stability
23%
Boron
22%
Igniter
22%
Liquid Water
21%
Premixed Methane
20%
Non-premixed
20%
Reynolds number
19%
Linear Burning Rate
19%
High Pressure
19%
Combustion Behavior
18%
Priming Event
18%
Water Mixtures
17%
Micron-sized Aluminum
17%
Constant Pressure
17%
Hydrocarbon Fuel
16%
Impingement Angle
16%
Injector
16%
Peak Pressure
16%
Low Pressure
16%
Hydrocarbons
16%
Airbag
16%
Pressure Dependence
15%
Pressure Range
15%
Flow Area
15%
Engineering
Burning Rate
100%
Ignition
75%
Oxidizer
73%
Solid Fuel
66%
Equivalence Ratio
65%
Reactant
61%
Rocket Engine
55%
Ignition Delay
47%
Diffusion Flame
43%
Methane
35%
Delay Time
29%
Strand
29%
Chamber Pressure
28%
Propulsion System
26%
Experimental Investigation
26%
Nanoscale
25%
Deflagration
25%
Energetics
21%
Mass Flowrate
21%
Flame Propagation
19%
Peak Pressure
18%
Flame Stability
18%
Hybrid Rocket Engine
17%
Pressure Range
17%
Reynolds' Number
17%
Fossil Fuel
17%
Flow Rate
17%
Initial Temperature
17%
Primary Flow
16%
Flow Area
15%
Transients
15%
Size of Particle
14%
Air Mixture
14%
Experimental Result
14%
Particle Diameter
13%
Secondary Flow
13%
Pressure Level
13%
Nanoparticle
13%
Internal Diameter
12%
Cold Flow
12%
Premixed Flame
11%
Borohydride
11%
Dilution
11%
Mass Fraction
11%
Gas-Phase
11%
Specific Impulse
11%
Dust Cloud
10%
