Keyphrases
Unburned Hydrocarbons
71%
Combustor
71%
Excimer Laser
57%
Atmospheric Pressure
50%
Tuneability
50%
Premixed
42%
Heptane
34%
Double-shell
31%
Prevaporized
28%
Swirl-stabilized
28%
Partially Premixed
28%
Laser-induced Fluorescence
26%
Combustion Process
24%
Aerothermodynamics
21%
Combustion Chamber
17%
Aeroengine Disk
14%
Nominal Stress Method
14%
Aero-engine Components
14%
Conical Shell
14%
Non-intrusive Measurement
14%
Law
14%
Mechanical Design
14%
Simplified Method
14%
Flow Direction
14%
Oblique Shock
14%
Laser-induced
14%
High Mass Loading
14%
Synoptic
14%
Elevated Pressure
14%
Flow Field
14%
Scramjet
14%
Computer Program
14%
Lifetime Estimation
14%
Lean Premixed Prevaporized Combustor
14%
Pressure Condition
14%
Laser-induced Fluorescence Imaging
14%
Axial Compressor
14%
Model Combustor
14%
Method Comparison
14%
Geometric Effect
14%
Aspect Ratio
14%
Axial Turbine
14%
Ratio Optimization
14%
KrF Excimer Laser
12%
Hydroxyl Radical
11%
248 Nm Excimer Laser
10%
Symmetry Line
10%
Imaging Techniques
10%
Vortex-induced
10%
Gaseous Fuel
10%
Engineering
Combustor
100%
Excimer Laser
85%
Atmospheric Pressure
71%
Flow Direction
32%
Aero-Engines
28%
Measuring Volume
28%
Image Signal
28%
Combustion Product
28%
Main Flow
28%
Broad Band
28%
Band Emission
28%
Flame Front
28%
Silicon Dioxide
23%
Flow Distribution
21%
Combustion Chamber
20%
Aerothermodynamics
16%
Illustrates
15%
Laser-Induced Fluorescence Imaging
14%
Axial Compressors
14%
Nominal Stress
14%
Experimental Investigation
14%
Elevated Pressure
14%
Conical Shell
14%
Mechanical Design
14%
Aspect Ratio
14%
Turbine
14%
Vortex
14%
Natural Gas
14%
Ignition
10%
Local Strain
9%
Oblique Shock
7%
Flexural Stiffness
7%
Fundamental Relation
7%
Reference Velocity
7%
Dimensional Flow
7%
Free Vortex
7%
Main Parameter
7%
Factor of Safety
7%
Centrifugal Stress
7%
Compressor Performance
7%
Rotor Blade
7%
Air Flow
5%