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Optimization of turboprop model #217

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merged 13 commits into from
Apr 2, 2024
Merged

Optimization of turboprop model #217

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6afb9e9
Turboprop thermodynamic equations rewrite
florentLutz Mar 22, 2024
3ba3b03
Nested turboprop sizing
florentLutz Mar 22, 2024
4cebd78
Nested geometry parameter
florentLutz Mar 22, 2024
86bd408
Nested thrust max problems
florentLutz Mar 22, 2024
0d73f2e
Max thrust rework
florentLutz Mar 26, 2024
f9aed1e
Nested fuel consumption problem
florentLutz Mar 26, 2024
9e5ff94
Fuel consumption problem implemented
florentLutz Mar 27, 2024
875cedd
Max power reworked
florentLutz Mar 28, 2024
d5e9ff1
Cleanup
florentLutz Mar 28, 2024
6330531
Test cache saturation
florentLutz Mar 28, 2024
54c2f5b
Map construction rework
florentLutz Mar 29, 2024
04c50cd
Integration test working
florentLutz Apr 2, 2024
63ccadd
Merge branch 'main' into dev_turboprop_optim
florentLutz Apr 2, 2024
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4 changes: 2 additions & 2 deletions integration_tests/oad_process/test_oad_process.py
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Original file line number Diff line number Diff line change
Expand Up @@ -154,10 +154,10 @@ def test_oad_process_tbm_900(cleanup):
_check_weight_performance_loop(problem)

# noinspection PyTypeChecker
assert_allclose(problem.get_val("data:mission:sizing:fuel", units="kg"), 765.0, atol=1)
assert_allclose(problem.get_val("data:mission:sizing:fuel", units="kg"), 768.0, atol=1)
assert_allclose(problem["data:handling_qualities:stick_fixed_static_margin"], 0.23, atol=1e-2)
# noinspection PyTypeChecker
assert_allclose(problem.get_val("data:weight:aircraft:MTOW", units="kg"), 3359.0, atol=1)
assert_allclose(problem.get_val("data:weight:aircraft:MTOW", units="kg"), 3362.0, atol=1)
# noinspection PyTypeChecker
assert_allclose(problem.get_val("data:weight:aircraft:OWE", units="kg"), 2114.0, atol=1)

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