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STAR
Cal STAR — firmware, DAQ server, and engine design
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Functions | |
| None | _clean_frozen (Dict[str, Any] req) |
| float | _sf (Any x) |
| Tuple[float, float] | _dp_ratios (Dict[str, Any] perf) |
| Tuple[float, float] | _cds (Dict[str, Any] perf) |
| str | _geom_row (Any opt_cfg) |
| None | main () |
Variables | |
| ROOT = Path(__file__).resolve().parents[1] | |
Sweep Layer-1 over target O/F and fuel tank pressure cap. Each run: free throat ±12.5%, R ∈ [0.85, 1.15], ΔP_inj/Pc ∈ [0.15, 0.40] both streams, target thrust 8000 N via ``design_requirements``, ``optimal_of_ratio`` sets MR target. Writes CSV under ``output/layer1_sweep_of_fuel_pressure.csv`` and prints a summary table.
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Definition at line 62 of file sweep_layer1_of_fuel_pressure.py.
References _sf().
Referenced by main().
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Definition at line 28 of file sweep_layer1_of_fuel_pressure.py.
Referenced by main().
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Definition at line 48 of file sweep_layer1_of_fuel_pressure.py.
Referenced by main().
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Definition at line 69 of file sweep_layer1_of_fuel_pressure.py.
Referenced by main().
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Definition at line 38 of file sweep_layer1_of_fuel_pressure.py.
| None sweep_layer1_of_fuel_pressure.main | ( | ) |
Definition at line 79 of file sweep_layer1_of_fuel_pressure.py.
References _cds(), _clean_frozen(), _dp_ratios(), _geom_row(), _sf(), and main().
Referenced by main().
| sweep_layer1_of_fuel_pressure.ROOT = Path(__file__).resolve().parents[1] |
Definition at line 20 of file sweep_layer1_of_fuel_pressure.py.