Designing propeller
Traceback (most recent call last):
File "c:\Users\ADMIN\OneDrive\Projects\capstone_project\Download\Tutorials-2.5.2\Tutorials-2.5.2\tut_eVTOL.py", line 592, in <module>
main()
File "c:\Users\ADMIN\OneDrive\Projects\capstone_project\Download\Tutorials-2.5.2\Tutorials-2.5.2\tut_eVTOL.py", line 35, in main
vehicle = setup_vehicle()
File "c:\Users\ADMIN\OneDrive\Projects\capstone_project\Download\Tutorials-2.5.2\Tutorials-2.5.2\tut_eVTOL.py", line 351, in setup_vehicle
propeller = propeller_design(propeller)
File "C:\Users\ADMIN\AppData\Local\Packages\PythonSoftwareFoundation.Python.3.9_qbz5n2kfra8p0\LocalCache\local-packages\Python39\site-packages\suave-2.5.2-py3.9.egg\SUAVE\Methods\Propulsion\propeller_design.py", line 130, in propeller_design
airfoil_data = compute_airfoil_polars(a_geo, a_pol,npoints = number_of_airfoil_section_points)
File "C:\Users\ADMIN\AppData\Local\Packages\PythonSoftwareFoundation.Python.3.9_qbz5n2kfra8p0\LocalCache\local-packages\Python39\site-packages\suave-2.5.2-py3.9.egg\SUAVE\Methods\Geometry\Two_Dimensional\Cross_Section\Airfoil\compute_airfoil_polars.py", line 155, in compute_airfoil_polars
CL2, CD2 = post_stall_coefficients(state,settings,geometry)
File "C:\Users\ADMIN\AppData\Local\Packages\PythonSoftwareFoundation.Python.3.9_qbz5n2kfra8p0\LocalCache\local-packages\Python39\site-packages\suave-2.5.2-py3.9.egg\SUAVE\Methods\Aerodynamics\AERODAS\post_stall_coefficients.py", line 87, in post_stall_coefficients
CL2[con3] = -0.032*(alpha[con3]/Units.deg-92.0) + RCL2*((alpha[con3]-92.*Units.deg)/(51.0*Units.deg))**N2
IndexError: too many indices for array: array is 1-dimensional, but 2 were indexed
Does anyone know why I am getting this error?
Thank you,
Yash