Added steady aero validation case, finished one
@@ -9,7 +9,7 @@ route = os.path.dirname(os.path.realpath(__file__)) + '/'
# flight conditions
u_inf = 10
rho = 1.225
-alpha = 5
+alpha = 20
beta = 0
c_ref = 1
b_ref = 16
@@ -50,7 +50,8 @@ momenty = 0
momentx = 0
# discretisation data
-num_elem_main = int(10*aspect_ratio/2)
+import math
+num_elem_main = math.ceil(10*aspect_ratio/2/2)*2
num_elem_tail = 5
num_elem_fin = 4
num_elem_fuselage = 10
@@ -69,7 +70,7 @@ num_node = num_node_main + (num_node_main - 1)
# num_node += num_node_fin - 1
nodes_distributed = num_node
-m_main = 8
+m_main = 16
m_tail = 5
m_fin = 5
