atest-flatplate2d-spalartallmaras.py File Reference

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Namespaces
	atest-flatplate2d-spalartallmaras

Variables
tuple	root = cf.Core.root()
tuple	env = cf.Core.environment()
tuple	model = root.create_component('NavierStokes', 'cf3.solver.ModelUnsteady')
	Global configuration. More...
tuple	domain = model.create_domain()
tuple	physics = model.create_physics('cf3.UFEM.NavierStokesPhysics')
tuple	solver = model.create_solver('cf3.UFEM.Solver')
tuple	nstokes = solver.add_unsteady_solver('cf3.UFEM.NavierStokes')
tuple	satm = solver.add_unsteady_solver('cf3.UFEM.SpalartAllmaras')
tuple	blocks = domain.create_component('blocks', 'cf3.mesh.BlockMesh.BlockArrays')
tuple	points = blocks.create_points(dimensions = 2, nb_points = 12)
tuple	block_nodes = blocks.create_blocks(6)
tuple	block_subdivs = blocks.create_block_subdivisions()
tuple	gradings = blocks.create_block_gradings()
tuple	inlet_patch = blocks.create_patch_nb_faces(name = 'inlet', nb_faces = 2)
tuple	bottom_patch1 = blocks.create_patch_nb_faces(name = 'bottom1', nb_faces = 1)
tuple	bottom_patch2 = blocks.create_patch_nb_faces(name = 'bottom2', nb_faces = 1)
tuple	bottom_patch3 = blocks.create_patch_nb_faces(name = 'bottom3', nb_faces = 1)
tuple	outlet_patch = blocks.create_patch_nb_faces(name = 'outlet', nb_faces = 2)
tuple	top_patch = blocks.create_patch_nb_faces(name = 'top', nb_faces = 3)
tuple	mesh = domain.create_component('Mesh', 'cf3.mesh.Mesh')
list	u_in = [1., 0.]
list	u_wall = [0., 0.]
float	NU_in = 0.001
int	NU_wall = 0
tuple	wall_distance = domain.create_component('WallDistance', 'cf3.mesh.actions.WallDistance')
tuple	bc = nstokes.get_child('BoundaryConditions')
tuple	time = model.create_time()
float	final_end_time = 0.5
float	save_interval = 0.1
int	iteration = 0