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STAR
Cal STAR — firmware, DAQ server, and engine design
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Functions | |
| test_published_anchors (r_over_d, l_over_d, expected, label) | |
| test_thin_plate_and_drilled_hole_are_not_the_same_number () | |
| test_length_factor_peaks_in_the_lichtarowicz_band () | |
| test_rounding_saturates () | |
| test_every_named_geometry_is_reachable_and_ordered (name) | |
| test_unset_leaves_the_old_path_untouched () | |
| test_filleting_one_side_is_a_real_trim () | |
| test_unknown_geometry_is_loud () | |
Variables | |
| _BASE | |
Cd comes from the orifice INLET and its L/d, and it is a per-side design knob. Two things this pins down. 1. THE ANCHORS. The widely-quoted "sharp-edged orifice, Cd = 0.61" is the THIN-PLATE value (L/d -> 0), where the jet leaves at the vena contracta and never recovers. The same sharp entry on a normally drilled hole (L/d 2-5) reattaches inside the bore and recovers to ~0.80. Conflating them under-predicts a real injector's flow by ~24%, which is the same class of error as the Cd-reduction loop this codebase already had. Sources: Huzel & Huang, "Modern Engineering for Design of Liquid-Propellant Rocket Engines" (injector orifice Cd table); Lichtarowicz, Duggins & Markland (1965), "Discharge Coefficients for Incompressible Non-Cavitating Flow through Long Orifices" (Cd peaks near L/d ~ 2, Re-independent above ~1e4); Nurick (1976) on inlet condition and cavitation inception. 2. IT IS A KNOB. `discharge.oxidizer` and `discharge.fuel` are separate config blocks, so filleting only ONE side's inlet raises that propellant's Cd and moves the momentum ratio / O/F without touching hole size, element count or angles.
| test_orifice_inlet_geometry_cd.test_every_named_geometry_is_reachable_and_ordered | ( | name | ) |
Definition at line 75 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_filleting_one_side_is_a_real_trim | ( | ) |
The knob: same hole, same dP, one side filleted -> that side flows measurably more.
Definition at line 89 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_length_factor_peaks_in_the_lichtarowicz_band | ( | ) |
Cd rises to a maximum near L/d ~ 2 and falls slowly after; it does not rise forever.
Definition at line 56 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_published_anchors | ( | r_over_d, | |
| l_over_d, | |||
| expected, | |||
| label ) |
Definition at line 44 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_rounding_saturates | ( | ) |
Past r/d ~ 0.2 rounding buys almost nothing -- why bellmouths are specified there.
Definition at line 65 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_thin_plate_and_drilled_hole_are_not_the_same_number | ( | ) |
The 24% gap is the whole point -- if these collapse, the model has lost the physics.
Definition at line 49 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_unknown_geometry_is_loud | ( | ) |
Definition at line 99 of file test_orifice_inlet_geometry_cd.py.
| test_orifice_inlet_geometry_cd.test_unset_leaves_the_old_path_untouched | ( | ) |
Opt-in: a config that declares no inlet geometry must behave exactly as before.
Definition at line 82 of file test_orifice_inlet_geometry_cd.py.
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protected |
Definition at line 34 of file test_orifice_inlet_geometry_cd.py.