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correct get avl aero coefs for static stability
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2 files changed

+4
-4
lines changed

2 files changed

+4
-4
lines changed

src/ceasiompy/PyAVL/func/results.py

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -127,7 +127,7 @@ def add_coefficients_in_aeromap(
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tixi = cpacs.tixi
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130-
cl, cd, cs, cmd, cml, cms, cmd_b, cms_a, cml_b = get_avl_aerocoefs(st_file_path)
130+
cd, cs, cl, cmd, cms, cml, cmd_b, cms_a, cml_b = get_avl_aerocoefs(st_file_path)
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plot = bool_(get_value(tixi, AVL_PLOTLIFT_XPATH))
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src/ceasiompy/PyAVL/tests/test_pyavl_results.py

Lines changed: 3 additions & 3 deletions
Original file line numberDiff line numberDiff line change
@@ -50,9 +50,9 @@ def test_get_avl_aerocoefs(self) -> None:
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0.00001,
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-0.66525,
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-0.00009,
53-
-0.156791,
54-
-24.343220,
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0.410176,
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-0.0027365191874944295,
54+
-0.424869339537334,
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0.007158921712660261,
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),
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)
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