Engineering
Combustor
100%
Rocket Engine
87%
Combined-Cycle Engine
63%
Combined Cycle
57%
Ignition
47%
Ejector
45%
Flow Distribution
40%
Mach Number
36%
Heat Release
34%
Vortex
31%
Combustion Product
27%
Combustion Chamber
27%
Experimental Investigation
23%
Mass Flowrate
23%
Experimental Result
22%
Specific Impulse
20%
Fuel Injection
20%
Two-Phase Flow
19%
Combustion Mode
18%
Isolators
15%
Propulsion System
15%
Diode Laser Absorption Spectroscopy
15%
Equivalence Ratio
15%
Air Flow
14%
Ignition Delay
14%
Shear Layer
14%
Ablation Rate
14%
Fossil Fuel
13%
Simulation Result
13%
Heat Flux
13%
Thermal Protection
13%
Numerical Model
13%
Supersonic Combustion
13%
Chemical Mechanism
13%
Burning Rate
13%
Delay Time
13%
Engine Performance
12%
Kinetic Model
12%
Vortex Shedding
11%
Good Agreement
11%
Thermal Environment
11%
Numerical Study
11%
Active Cooling
11%
Dump Combustor
10%
Flow Path
10%
Particle Trajectory
10%
Flow Velocity
10%
Active Control
9%
Cooling Channel
9%
Axisymmetric
9%
Material Science
Solid Propellant
38%
Surface (Surface Science)
33%
Composite Material
31%
Mach Number
23%
Aluminum
21%
Radiographic Testing
18%
Two Phase Flow
18%
Carbon Carbon Composites
13%
Boron
13%
Phase Change Material
10%
HTPB Propellant
9%
HMX
9%
Composite Propellant
8%
Coolant
7%
Density
7%
Carbon Dioxide
6%
Scanning Electron Microscopy
6%
Thermal Conductivity
5%
Large Eddy Simulation
5%
Natural Convection
5%
Aluminum Oxide
5%
Thermal Load
5%
