side slip support
@@ -110,7 +110,7 @@ class FlyingWing():
pass
### other params
- self.u_inf_direction=np.array([1.,0.,0.])
+ self.u_inf_direction=np.array([1.,np.sin(beta*np.pi/180),0.])
self.gravity_on = True
# aeroelasticity
@@ -423,11 +423,10 @@ class FlyingWing():
'structural_solver_settings': {'print_info': 'off',
'max_iterations': 150,
'num_load_steps': 4,
- 'delta_curved': 1e-5,
- 'min_delta': 1e-5,
+ 'delta_curved': 1e-1,
+ 'min_delta': 1e-10,
'gravity_on': self.gravity_on,
- 'gravity': 9.754,
- 'orientation': self.quat},}
+ 'gravity': 9.754}}
config['LinearUvlm'] = { 'dt': self.dt,
'integr_order': 2,
@@ -475,7 +474,7 @@ class FlyingWing():
'gust_shape': 'continuous_sin',
'gust_length': self.gust_length,
'gust_intensity': self.gust_intensity * self.u_inf,
- 'offset': 5.0,
+ 'offset': 15.0,
'span': self.main_chord * self.aspect_ratio},
# 'velocity_field_generator': 'SteadyVelocityField',
# 'velocity_field_input': {'u_inf': self.u_inf*1,
