nozzle.py File Reference

Go to the source code of this file.

Namespaces
namespace	engine
namespace	engine.core
namespace	engine.core.nozzle

Functions
Optional[float]	engine.core.nozzle.contraction_ratio_of (cg)
float	engine.core.nozzle.nozzle_stagnation_loss (Optional[float] contraction_ratio, float gamma)
float	engine.core.nozzle.expansion_ratio_for_exit_pressure (CEACache cea_cache, float MR, float Pc, float Pe, Optional[float] contraction_ratio=None)
dict	engine.core.nozzle.calculate_thrust (float Pc, float MR, float mdot_total, CEACache cea_cache, Any config, float Pa=101325.0, Optional[Dict] reaction_progress=None, bool debug=False)