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Improved continuum modeling of low density hypersonic flows
Sandeep Nijliawan
,
Graham V. Candler
, Deepak Bose
, Iain D. Boyd
Aerospace Engineering and Mechanics
Research output
:
Contribution to conference
›
Paper
›
peer-review
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Keyphrases
Hypersonic Flow
100%
Continuum Modeling
100%
Low Density
100%
Gasses
100%
Shock Waves
66%
Shock
33%
Direct Simulation Monte Carlo
33%
Thermal Conductivity
33%
Monte Carlo Calculation
33%
Translational Energy
33%
Thermal Energy
33%
Conservation Equations
33%
Intermolecular Potential
33%
Energy Relaxation
33%
Lias
33%
Translational Nonequilibrium
33%
Inverse Power
33%
Modeling Approaches
33%
Thermal Viscosity
33%
Thermal Rates
33%
Physics
Shock Wave
100%
Hypersonic Flow
100%
Continuum Modeling
100%
Thermal Conductivity
50%
Monte Carlo Calculation
50%