pymead.analysis.calc_aero_data

Functions

calculate_CPK_mses(analysis_subdir[, ...])	A specialized function that calculates the mechanical flow power coefficient for an underwing trailing edge aero-propulsive configuration.
calculate_CPK_mses_inviscid_only(analysis_subdir)	Calculates the mechanical flower power coefficient input to the control volume across the airfoil system control surface.
calculate_CPK_mses_old(analysis_subdir[, ...])	A specialized function that calculates the mechanical flow power coefficient for an underwing trailing edge aero-propulsive configuration.
calculate_CPK_power_consumption(analysis_subdir)	A specialized function that calculates the mechanical flow power coefficient
calculate_CPK_power_consumption_old(...)	A specialized function that calculates the mechanical flow power coefficient for an underwing trailing edge aero-propulsive configuration.
calculate_Cl_alfa_xfoil_inviscid(...)
calculate_Cl_integral_form(x, y, Cp, alfa)
calculate_aero_data(conn, airfoil_coord_dir, ...)	Convenience function calling either XFOIL or MSES depending on the tool specified
convert_cell_centered_to_edge_centered(...)
convert_xfoil_string_to_aero_data(line1, ...)	Extracts aerodynamic data from strings pulled from XFOIL log files.
extrapolate_data_line_mses_field(...[, ...])
line_integral_CPK_bl(rhoe_rhoinf, ue_uinf, ...)	Computes CPK at a given boundary layer location
line_integral_CPK_inviscid(Cp_up, Cp_down, ...)	Computes the mechanical flow power line integral in the inviscid streamtube only according to Drela's "Power Balance in Aerodynamic Flows", a 2009 AIAA Journal article
line_integral_CPK_inviscid_old(Cp, rho, u, ...)	Computes the mechanical flow power line integral in the inviscid streamtube only according to Drela's "Power Balance in Aerodynamic Flows", a 2009 AIAA Journal article
line_integral_Edot_inviscid(Cp, rho, u, v, ...)	.
line_integral_Edota_inviscid_TP(rho, u, v, x, y)	.
line_integral_Edotp_inviscid_TP(Cp, u, v, x, y)	.
read_alfa_from_xfoil_cp_file(xfoil_cp_file)
run_mplot(name, base_dir, mplot_settings[, ...])	A Python API for MPLOT
run_mses(name, base_folder, mses_settings, ...)	A Python API for MSES
run_mset(name, base_dir, mset_settings, ...)	A Python API for MSET
run_xfoil(airfoil_name, base_dir, ...[, ...])
shock_dissipation(x_edge, y_edge, u, v, M, ...)
surface_dissipation(last_BL_point)	Eq.
update_mses_settings_from_stencil(...)	Updates the MSES settings dictionary from a given multipoint stencil and multipoint index
update_xfoil_settings_from_stencil(...)	Updates the XFOIL settings dictionary from a given multipoint stencil and multipoint index
viscous_Edot(last_BL_point)	Eq.
write_blade_file(name, base_dir, ...)	Writes airfoil geometry to an MSES blade file
write_gridpar_file(name, base_folder, ...)	Writes grid parameters to a file readable by MSES
write_input_file(input_file, input_list)	Writes inputs from a list to a file for use as STDIN commands to the shell/terminal.
write_mses_file(name, base_folder, ...)	Writes MSES flow parameters to a file

Exceptions

ConvergenceFailedError
GeometryError