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Multi-spectral shocklayer radiance from a hypersonic slender body
Deborah A. Levin
,
Graham V. Candler
Aerospace Engineering and Mechanics
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
Hypersonic
100%
Vibrational States
100%
Radiance
100%
Slender Body
100%
Overlay Method
66%
Spatial Distribution
33%
Shock
33%
State-specific
33%
Hypersonic Vehicle
33%
Mid-infrared
33%
Expanding Flow
33%
Flow Modeling
33%
State Distribution
33%
Ambient CO2
33%
Specific Model
33%
Radiator
33%
Boltzmann Distribution
33%
Sounding Rocket Experiment
33%
Chemically Reacting
33%
Spectral Prediction
33%
Accurately Model
33%
Physics
Hypersonics
100%
Slender Body
100%
Carbon Dioxide
100%
Vibrational State
75%
Hypersonic Vehicle
25%
Boltzmann Distribution
25%
Spatial Distribution
25%
Engineering
Slender Body
100%
Carbon Dioxide
100%
Boltzmann Distribution
25%
Spatial Distribution
25%
Hypersonic Vehicle
25%