graphite_cooling.py File Reference

Go to the source code of this file.

Namespaces
namespace	engine
namespace	engine.pipeline
namespace	engine.pipeline.thermal
namespace	engine.pipeline.thermal.graphite_cooling

Functions
Dict[str, object]	engine.pipeline.thermal.graphite_cooling.carbon_oxidation (float T_s, float P_static, Dict[str, float] composition, float MW_mix, float g0, GraphiteInsertConfig cfg)
Dict[str, object]	engine.pipeline.thermal.graphite_cooling.graphite_surface_state (float T_s, gas, contour, Dict[str, float] composition, GraphiteInsertConfig cfg)
float	engine.pipeline.thermal.graphite_cooling.calculate_throat_heuristic_multiplier (float chamber_pressure, float chamber_velocity, float throat_velocity, float chamber_heat_flux, float gamma=1.2)
Dict[str, float]	engine.pipeline.thermal.graphite_cooling.compute_graphite_recession (float net_heat_flux, float throat_temperature, float gas_temperature, GraphiteInsertConfig graphite_config, float throat_area, float pressure, Optional[float] gas_density=None, Optional[float] gas_viscosity=None, Optional[float] oxygen_mass_fraction=None, Optional[float] characteristic_length=None, Optional[float] gas_velocity=None, Optional[float] heat_transfer_coefficient=None, Optional[float] backside_temperature=None, Optional[float] effective_thickness=None, gas_state=None, contour=None, Optional[Dict[str, float]] throat_composition=None)

Variables
float	engine.pipeline.thermal.graphite_cooling.R_GAS = 8.314462618
float	engine.pipeline.thermal.graphite_cooling.MW_C = 12.0107
float	engine.pipeline.thermal.graphite_cooling.ATM = 101325.0
dict	engine.pipeline.thermal.graphite_cooling.CARBON_OXIDISERS