chamber_geometry.py File Reference

Go to the source code of this file.

Namespaces
namespace	engine
namespace	engine.core
namespace	engine.core.chamber_geometry

Functions
	engine.core.chamber_geometry.area_exit_calc (diameter_exit=diameter_exit_default)
	engine.core.chamber_geometry.expansion_ratio_calc (area_exit, area_throat)
	engine.core.chamber_geometry.area_throat_calc (pc_design, thrust_design, force_coeffcient=force_coeffcient_default)
	engine.core.chamber_geometry.chamber_volume_calc (area_throat, l_star=l_star_default)
	engine.core.chamber_geometry.contraction_ratio_calc (area_chamber, area_throat)
	engine.core.chamber_geometry.area_chamber_calc (diameter_inner=chamber_diameter_default)
	engine.core.chamber_geometry.chamber_diameter_calc (area_chamber)
	engine.core.chamber_geometry.entrance_arc_volume (R_t, theta=theta_default, steps=4000)
	engine.core.chamber_geometry.chamber_length_calc (chamber_volume, area_throat, contraction_ratio, theta=theta_default)
	engine.core.chamber_geometry.contraction_length_horizontal_calc (area_chamber, entrance_arc_start_y, theta=theta_default)
	engine.core.chamber_geometry.generate_nozzle (area_throat, area_exit, steps=200, theta=theta_default)
	engine.core.chamber_geometry.chamber_geometry_calc (pc_design, thrust_design, force_coeffcient=force_coeffcient_default, diameter_inner=chamber_diameter_default, diameter_exit=diameter_exit_default, l_star=l_star_default, do_plot=False, color_segments=False, steps=200, export_dxf=None, theta=theta_default)

Variables
bool	engine.core.chamber_geometry.HAS_EZDXF = True
int	engine.core.chamber_geometry.theta_default = np.pi/4
float	engine.core.chamber_geometry.force_coeffcient_default = 1.4
int	engine.core.chamber_geometry.diameter_exit_default = 4 / 39.37
float	engine.core.chamber_geometry.l_star_default = 1.27
float	engine.core.chamber_geometry.chamber_diameter_default = 3.4 / 39.37
	engine.core.chamber_geometry.pts
	engine.core.chamber_geometry.data
	engine.core.chamber_geometry.lengths
	engine.core.chamber_geometry.pc_design
	engine.core.chamber_geometry.e6
	engine.core.chamber_geometry.thrust_design
	engine.core.chamber_geometry.do_plot
	engine.core.chamber_geometry.True
	engine.core.chamber_geometry.color_segments
	engine.core.chamber_geometry.export_dxf