Radiative-collisional models in non-equilibrium aerothermodynamics of entry probes

Journal of Heat Transfer

Volumn 134, Issue 3, 2012, Pages

  Surzhikov, Sergey T ^a  

^a INSTITUTE FOR PROBLEMS IN MECHANICS   (Russian Federation)

Author keywords

aerothermodynamics; entry probes; radiative collisional models

Indexed keywords

ACCURATE PREDICTION; AEROTHERMODYNAMICS; CHEMICAL COMPOSITIONS; CHEMICAL PROCESS; COMPUTATIONAL CODES; DESIGN SPACES; DIATOMIC MOLECULES; ELECTRONIC KINETIC; EQUILIBRIUM THERMODYNAMICS; GAS FLOWS; GEO-STATIONARY ORBITS; GOVERNING EQUATIONS; HIGH ALTITUDE; HIGH TEMPERATURE; IONIZED GAS; LARGE PARTS; LOCAL THERMODYNAMIC EQUILIBRIUM; LOW TEMPERATURE PLASMAS; NASA MISSIONS; NEW YORK; NON EQUILIBRIUM; NON-EQUILIBRIUM EFFECTS; NONEQUILIBRIUM CONDITIONS; NUMERICAL SIMULATION ALGORITHMS; PHYSICAL MODEL; PHYSICO-CHEMICALS; RADIATIVE HEAT LOADS; RADIATIVE HEATING; SPACE MISSIONS; SPACE VEHICLES; SPECTRAL RADIATION; THERMOCHEMICAL DESTRUCTION;

AEROSPACE APPLICATIONS; ATMOSPHERIC DENSITY; CARBON DIOXIDE; COLLISIONAL PLASMAS; COMPUTATIONAL FLUID DYNAMICS; FORECASTING; GAS MIXTURES; GASES; GEOCHEMISTRY; HEAT TRANSFER; HYPERSONIC FLOW; IONIZATION OF GASES; KINETICS; MIXTURES; MODELS; MOON; NASA; PARKS; PROBES; SPACE FLIGHT; TEMPERATURE; TRANSPORT PROPERTIES; VEHICLES;

COMPUTER SIMULATION;

EID: 84855813620     PISSN: 00221481     EISSN: 15288943     Source Type: Journal    
DOI: 10.1115/1.4005127     Document Type: Article

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