correct get avl aero coefs for static stability

Author: LeonDeligny

src/ceasiompy/PyAVL/func/results.py

@@ -127,7 +127,7 @@ def add_coefficients_in_aeromap(
 
     tixi = cpacs.tixi
 
-    cl, cd, cs, cmd, cml, cms, cmd_b, cms_a, cml_b = get_avl_aerocoefs(st_file_path)
+    cd, cs, cl, cmd, cms, cml, cmd_b, cms_a, cml_b = get_avl_aerocoefs(st_file_path)
 
     plot = bool_(get_value(tixi, AVL_PLOTLIFT_XPATH))
 

src/ceasiompy/PyAVL/tests/test_pyavl_results.py

@@ -50,9 +50,9 @@ def test_get_avl_aerocoefs(self) -> None:
                 0.00001,
                 -0.66525,
                 -0.00009,
-                -0.156791,
-                -24.343220,
-                0.410176,
+                -0.0027365191874944295,
+                -0.424869339537334,
+                0.007158921712660261,
             ),
         )