minor changes in docs for steplinearuvlm
@@ -21,6 +21,7 @@ class StepLinearUVLM(BaseSolver):
is the case of an aeroelastic solver, where the setting below would be parsed through ``aero_solver_settings``.
Notes:
+
The ``integr_order`` variable refers to the finite differencing scheme used to calculate the bound circulation
derivative with respect to time :math:`\dot{\mathbf{\Gamma}}`. A first order scheme is used when
``integr_order == 1``
@@ -38,7 +39,8 @@ class StepLinearUVLM(BaseSolver):
* Thence, rotates by the same quantity as the FoR ``A``.
- It is resemblant of a stability axes and is recommended any time rigid body dynamics are included.
+
+ It is similar to a stability axes and is recommended any time rigid body dynamics are included.
See Also:
:class:`sharpy.sharpy.linear.assembler.linearuvlm.LinearUVLM`
@@ -112,9 +114,6 @@ class StepLinearUVLM(BaseSolver):
scaling_settings_description)
def __init__(self):
- """
- Read default settings from linuvlm module
- """
self.data = None
self.settings = None
self.lin_uvlm_system = None
@@ -284,8 +283,7 @@ class StepLinearUVLM(BaseSolver):
The linear UVLM system is then solved as detailed in :func:`sharpy.linear.src.linuvlm.Dynamic.solve_step`.
The output is a column vector containing the aerodynamic forces at the panel vertices.
- To Do:
- Option for impulsive start?
+ To Do: option for impulsive start?
Args:
aero_tstep (AeroTimeStepInfo): object containing the aerodynamic data at the current time step
@@ -434,9 +432,6 @@ class StepLinearUVLM(BaseSolver):
f_aero = y_n
gamma_vec, gamma_star_vec, gamma_dot_vec = self.data.aero.linear['System'].unpack_state(x_n)
- # gamma_vec = self.data.aero.linear['gamma_0'] + dgamma_vec
- # gamma_star_vec = self.data.aero.linear['gamma_star_0'] + dgamma_star_vec
- # gamma_dot_vec = self.data.aero.linear['gamma_dot_0'] + dgamma_dot_vec
# Reshape output into forces[i_surface] where forces[i_surface] is a (6,M+1,N+1) matrix and circulation terms
# where gamma is a [i_surf](M+1, N+1) matrix
