NACA .stl airfoil generator Python Application

Related Resources: calculators

NACA .stl airfoil generator Python Application

Python Script which directly generates a 4-digit NACA profile in .STL ASCII code file.

Python code - This application requires knowledge of Python installation and code execution.

NOTE:

Refunds are not awarded after Python files have been downloaded - review your membership agreement for details.
Units (if utilized) utilized within calculators are either SI or Imperial (some enable both SI and Imperial) and member (you) are responsible for conversions. Ensure that you verify units utilized in excel application meet your requirements before downloading.

Premium Membership Required for download

Download: NNACA .stl airfoil file generator

Output

NACA Airfoil

Python Code Execution Data:

Variables:
- "foil" - number
- "numberOfPoints" - cnt
- "chordLength" - meter
- "lenght" - meter
- "angleOfAttack" - deg

Example

python myNaca.py 2412 150 1 3 6

Defualt

python myNaca.py

Output Examples

Source

Python code - This application requires knowledge of Python installation and code execution.

No requirements outside the Python Standard Library

Support:

Engineers Edge has tested the basic functions and operation of this application using Python 3.11.9 and supporting modules.
Supporting Windows application "Visual Studio Code".
THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE.