Rename pazi to pazy
@@ -1104,11 +1104,13 @@ class QuasiInfinite(FlyingWing):
self.elem_stiffness = np.zeros((self.num_elem_tot,), dtype=int)
self.elem_mass = np.zeros((self.num_elem_tot,), dtype=int)
-class Pazi(FlyingWing):
+class Pazy(FlyingWing):
'''
- Build a Pazi wing.
- This class is nothing but a FlyingWing with pre-defined geometry properties
- and mass/stiffness data ("update_mass_stiffness" method)
+ Build a Pazy wing.
+
+ The Pazy wing is a highly flexible wing designed and developed at Technion University as an aeroelastic
+ test case.
+
'''
def __init__(self,
@@ -1127,7 +1129,7 @@ class Pazi(FlyingWing):
n_surfaces=1,
physical_time=2,
route='.',
- case_name='pazi',
+ case_name='pazy',
RollNodes=False):
super().__init__(M=M, N=N,
Mstar_fact=Mstar_fact,
@@ -1173,7 +1175,7 @@ class Pazi(FlyingWing):
sigma_scale_I = 1
# Pulling:
- ea = 7.12E+06 # Typo corrected
+ ea = 7.12E+06
# In-plane bending:
ga_inp = 3.31E+06
@@ -1257,7 +1259,7 @@ class Pazi(FlyingWing):
-class PaziControlSurface(Pazi):
+class PazyControlSurface(Pazy):
def __init__(self,
M, N, # chord/span-wise discretisations
@@ -1277,7 +1279,7 @@ class PaziControlSurface(Pazi):
n_surfaces=1,
physical_time=2,
route='.',
- case_name='pazi',
+ case_name='pazy',
RollNodes=False):
super().__init__(M=M, N=N,
