Compute Panel Dimensions in TACS for Stiffened Panel Optimizations (#339

)

* fix typo in test bdf utils callbacks

* update the nlbgs driver

* fix plot_manager with new history file setup

* update the plot manager function

* update the tacs interface to work with panel length and width constraints

* add temp debug statements to tacs interface for ML oneway opt

* fix sparse gradients for panel length, width in tacs closed form

* update the oneway struct driver to make init transfer default true

* fix the sparse gradient for adjacency constraints

* remove some of the print statements

* remove printouts in funtofem

* make sparse opt manager default True

* remove plot hist with option

* fix linear gradients in pyoptsparse

* add new sparse linear constraint settings for efficient memory management

* None checks

funtofem/driver/oneway_struct_driver.py

@@ -538,6 +538,7 @@ def _transfer_fixed_aero_loads(self):
                 # the mesh for the new structural shape
                 body.transfer_loads(scenario)
                 body.transfer_heat_flux(scenario)
+
         return
 
     def solve_forward(self):