test_nozzle_cea_basis.py File Reference

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Namespaces
namespace	test_nozzle_cea_basis

Functions
	test_nozzle_cea_basis._python_physics (monkeypatch)
	test_nozzle_cea_basis.runner ()
	test_nozzle_cea_basis.test_exit_pressure_is_ceas_shifting_equilibrium (runner)
	test_nozzle_cea_basis.test_ambient_matched_expansion_ratio (runner)
	test_nozzle_cea_basis.test_runner_exit_state_is_on_the_thrust_basis (runner)
	test_nozzle_cea_basis.test_rayleigh_loss_matches_ceas_finite_area_combustor (CR, ceas)
	test_nozzle_cea_basis.test_demand_uses_the_nozzle_stagnation_pressure ()
	test_nozzle_cea_basis.test_cache_ambient_coefficient_uses_the_ambient_it_is_given (runner)
	test_nozzle_cea_basis.test_cache_flags_what_it_clamps (runner)
	test_nozzle_cea_basis.test_geometry_fallback_sizes_the_throat_on_the_delivered_basis (runner)

Variables
	test_nozzle_cea_basis.ROOT = os.path.dirname(os.path.dirname(os.path.abspath(__file__)))
	test_nozzle_cea_basis.CFG = os.path.join(ROOT, "configs", "ethalox_6500N.yaml")
float	test_nozzle_cea_basis.PSI = 6894.757293168361
float	test_nozzle_cea_basis.P_TANK = 584.27 * PSI