make_naca_propeller_blade_rsolid
Kind: Function
Domain: Modeling and geometry
Canonical import: from cadflow import make_naca_propeller_blade_rsolid
Signature
def make_naca_propeller_blade_rsolid(blade_length=5.0, root_chord=1.5, tip_chord=0.3, total_twist_angle=45.0, num_sections=7, t_c=0.16) -> cadflow._engine.geometry.core.Solid
Description
Create a single propeller blade solid from a twisted NACA 0016 profile. The blade root starts at the origin and extends along +Z.
Parameters
| Name | Type | Required | Default | Source description |
|---|---|---|---|---|
blade_length | Any | no | 5.0 | Not explicitly described in the source docstring. |
root_chord | Any | no | 1.5 | Not explicitly described in the source docstring. |
tip_chord | Any | no | 0.3 | Not explicitly described in the source docstring. |
total_twist_angle | Any | no | 45.0 | Not explicitly described in the source docstring. |
num_sections | Any | no | 7 | Not explicitly described in the source docstring. |
t_c | Any | no | 0.16 | Not explicitly described in the source docstring. |
Returns
Type: cadflow._engine.geometry.core.Solid
The source docstring does not declare additional return semantics.
Errors
The source docstring does not declare a narrower exception contract. Invalid types, values, ownership, paths, or backend state may still raise the corresponding public error.
Behavior and constraints
- The contract below is generated from the current public runtime signature. Check domain notes for ownership and workflow constraints.
Import check
from cadflow import make_naca_propeller_blade_rsolid