STAR
Cal STAR — firmware, DAQ server, and engine design
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pareto_throat_dp_pressures.py File Reference

Go to the source code of this file.

Namespaces

namespace  pareto_throat_dp_pressures

Functions

List[Tuple[float, float]] pareto_throat_dp_pressures._parse_tank_scenarios (str s)
float pareto_throat_dp_pressures._throat_center_mm2 (Any cfg)
None pareto_throat_dp_pressures._apply_throat_mm2 (Any cfg, float mm2)
Dict[str, Any] pareto_throat_dp_pressures._row_eval (PintleEngineRunner runner, float P_O_psi, float P_F_psi, float F_t, float MR_t)
Tuple[Optional[np.ndarray], float, int] pareto_throat_dp_pressures._solve_pressures (PintleEngineRunner runner, float F_t, float MR_t, Tuple[float, float] b_o, Tuple[float, float] b_f, *, bool de_fallback, int de_maxiter, int de_pop, int maxfun_local, bool quick_local)
List[Dict[str, Any]] pareto_throat_dp_pressures._pareto_nd (Sequence[Dict[str, Any]] rows, *, float m_err_cap)
None pareto_throat_dp_pressures.main ()

Variables

 pareto_throat_dp_pressures.ROOT = Path(__file__).resolve().parents[1]
float pareto_throat_dp_pressures.PSI_TO_PA = 6894.76