They are tabulated Cl/Cd coefficients of an airfoil. I want to model a turbine blade in a simple domain without the need to actually mesh the turbine geometry (by using momentum source terms).
I figured that the following code works fine except that it gives me a warning while compiling it:
real data ;
host_to_node_real (data,6) ;
warning C4047: 'function': 'double *' differs in levels of indirection from 'real '
warning C4047: 'mphost_to_node_double': different types for formal and actual parameter 1