Engineering
Activation Energy
10%
Axisymmetric
12%
Backpressure
8%
Burned Gas
19%
Combustion Chamber
14%
Combustion Mode
9%
Combustor
83%
Computational Fluid Dynamics
8%
Computer Simulation
16%
Concentration Gradient
8%
Degree of Freedom
11%
Detonation Wave
74%
Dilution
8%
Energy Engineering
11%
Engine Performance
11%
Engine System
19%
Equivalence Ratio
16%
Euler Equation
8%
Flight Condition
8%
Flight Test
13%
Frequency Operation
10%
Heat Release
13%
Ignition
14%
Initial Pressure
23%
Interior Ballistics
13%
Mass Flowrate
14%
Methane
9%
Numerical Study
11%
One Dimensional
27%
Oscillatory
10%
Oxidizer
23%
Premixed Flame
16%
Pressure Ratio
12%
Propagation Velocity
11%
Propellant Gas
8%
Propulsion System
11%
Pulse Detonation Engines
24%
Purge Gas
15%
Reacting Flow
8%
Reaction Model
25%
Rocket Engine
39%
Rotary Valve
22%
Rotating Detonation
41%
Rotating Detonation Engine
100%
Shock Front
18%
Simulation Result
23%
Specific Impulse
28%
Stagnation Streamline
10%
Supersonic Combustion
14%
Two Dimensional
26%
Keyphrases
Aerospike Nozzle
6%
Closure Space
6%
Cylindrical Projectile
6%
Detonation
6%
Detonation Engine
17%
Detonation Wave
16%
Engine Development
6%
Engine System
12%
Equivalence Ratio
6%
Ethylene
5%
Flight Demonstration
13%
Flight Measurements
6%
Flow Features
7%
Four Cylinders
11%
Ground Test
9%
Hypersonic
11%
Hypersonic Projectiles
6%
Igniter
5%
Liquid Propellant
5%
Non-premixed Flame
5%
Nozzle
7%
Nozzle Flow
6%
Nuclear Fuel Cycle Facilities
6%
Numerical Investigation
10%
Oblique Detonation Wave
13%
Oxidizer
6%
PDR System
6%
Plane Plate
6%
Pressure History
6%
Projectile Acceleration
7%
Propellant
9%
Pulse Detonation
13%
Pulse Detonation Engine
10%
Pulse Detonation Rocket Engine
11%
Purge Gas
6%
Reaction Control System
6%
Reflection Phenomena
6%
Rocket
10%
Rotary
10%
Rotary Valve
11%
Rotating Detonation Engine
11%
Shock-induced Combustion
9%
Solid Propellant
6%
Solid-gas
6%
Sounding Rocket
10%
Specific Impulse
7%
Spherical Projectile
9%
Thrust Measurement
10%
Thrust-to-weight Ratio
6%
Velocity Oscillation
5%
