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Distributed combustion response function modeling and measurement
E. H. Cardiff
, M. M. Micci
Aerospace Engineering
Materials Research Institute (MRI)
Research output
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Contribution to conference
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Paper
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peer-review
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Keyphrases
Response Function
100%
Function Modeling
100%
Combustion Response
100%
Distributed Combustion
100%
Aluminum Particles
33%
Acoustic Conditions
33%
Magnetic Flowmeter
33%
Simultaneous Measurement
16%
Acoustics
16%
Flow Testing
16%
Rocket
16%
Numerical Model
16%
Acoustic Pressure
16%
Acoustic Waves
16%
Transverse Velocity
16%
Combustion Chamber
16%
Velocity Oscillation
16%
Solid Propellant
16%
Acoustic Velocity
16%
Flow Environment
16%
Combustion Model
16%
Acoustic Modeling
16%
Cold Flow
16%
Velocity Coupled Response
16%
Toothed Gear
16%
Time Expressions
16%
Aluminum Combustion
16%
Burning Time
16%
Choked Nozzle
16%
Engineering
Response Function
100%
Flowmeter
100%
Experimental Result
50%
Acoustic Pressure
50%
Numerical Model
50%
Cold Flow
50%
Developed Expression
50%
Transversal Velocity
50%
Burn Time
50%
Combustion Chamber
50%
Physics
Flowmeter
100%
Magnetism
100%
Acoustic Wave
50%
Solid Propellant
50%
Acoustic Velocity
50%
Numerical Model
50%
Combustion Chamber
50%
Acoustics
50%