flds_steady_aerodyn_forceq_cre | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, force, moment, force_type ) |
Description: | ||
This function creates the Aerodynamic Force/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Force/Q vector |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | force | The id of the Force field |
INTEGER | moment | The id of the Moment field |
STRING | force_type | Force Type: “Structural” or “Aero” |
Output: | ||
None. |
flds_steady_aerodyn_forceq_get | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, force, moment, force_type ) |
Description: | ||
This function gets the data for the specified Aerodynamic Force/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Force/Q vector to get |
Output: | ||
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | force | The id of the Force field |
INTEGER | moment | The id of the Moment field |
STRING | force_type | Force Type: “Structural” or “Aero” |
flds_steady_aerodyn_forceq_mod | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, force, moment, force_type ) |
Description: | ||
This function modifies the specified Aerodynamic Force/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Force/Q vector to modify |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | force | The id of the Force field |
INTEGER | moment | The id of the Moment field |
STRING | force_type | Force Type: “Structural” or “Aero” |
Output: | ||
None. |
flds_steady_aerodyn_nwashq_cre | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, norm_wash ) |
Description: | ||
This function creates the Aerodynamic Normalwash/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Normalwash/Q vector |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | norm_wash | The id of the Normalwash field |
Output: | ||
None. |
flds_steady_aerodyn_nwashq_get | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, norm_wash ) |
Description: | ||
This function gets the data for the specified Aerodynamic Normalwash/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Normalwash/Q vector to get |
Output: | ||
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | norm_wash | The id of the Normalwash field |
flds_steady_aerodyn_nwashq_mod | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, norm_wash ) |
Description: | ||
This function modifies the specified Aerodynamic Normalwas/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Normalwash/Q vector to modify |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | norm_wash | The id of the Normalwash field |
Output: | ||
None. |
flds_steady_aerodyn_pressq_cre | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, top_pres, bot_pres, num_box ) |
Description: | ||
This function creates the Aerodynamic Pressure/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Pressure/Q vector |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | top_pres | The id of the Top Surface Pressure field |
INTEGER | bot_pres | The id of the Bottom/Delta Surface Pressure field |
INTEGER | num_box | A flag identifying if both the Top and the Bottom Pressure |
Output: | ||
None. |
flds_steady_aerodyn_pressq_get | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, top_pres, bot_pres, num_box ) |
Description: | ||
This function gets the data for the specified Aerodynamic Pressure/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Pressure/Q vector to get |
Output: | ||
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | top_pres | The id of the Top Surface Pressure field |
INTEGER | bot_pres | The id of the Bottom/Delta Surface Pressure field |
INTEGER | num_box | A flag identifying if both the Top and the Bottom Pressure |
flds_steady_aerodyn_pressq_mod | ( vector_name, coord_label, xz_sym, xy_sym, mach_num, num_of_rbm, rbm_values, num_of_cntrl_devs, cntrl_dev_values, lbc_set_sf, top_pres, bot_pres, num_box ) |
Description: | ||
This function modifies the specified Aerodynamic Pressure/Q vector. | ||
Input: | ||
STRING | vector_name | Name of the Pressure/Q vector to modify |
INTEGER | coord_label | The label of the coordinate frame |
INTEGER | xz_sym | The label of the XZ Symmetry |
INTEGER | xy_sym | The label of the XY Symmetry |
REAL | mach_num | The Mach number |
INTEGER | num_of_rbm | The number of Rigid Body Motions defined |
REAL | rbm_values() | Array of all the defined Rigid Body Motion values |
INTEGER | num_of_cntrl_devs | The number of Control Devices defined. This includes General Controllers and both the linear and nonlinear Control Surfaces. |
REAL | cntrl_dev_values() | Array of all the defined Control Device values |
REAL | lbc_set_sf | The Load.BC Set Scale Factor |
INTEGER | top_pres | The id of the Top Surface Pressure field |
INTEGER | bot_pres | The id of the Bottom/Delta Surface Pressure field |
INTEGER | num_box | A flag identifying if both the Top and the Bottom Pressure |
Output: | ||
None. |