Implement any regression model to predict the self noise generated by an airfoil using various features provided.Target output is sound level in decibels.
1.Frequency, in Hertzs.
2.Angle of attack, in degrees.
3.Chord length, in meters.
4.Free-stream velocity, in meters per second.
5.Suction side displacement thickness, in meters.
Add your solution file to 'machineLearning/33' folder. The path for your solution file should look like this:
/machineLearning/33/<your_solution_file>
Note
Please claim the issue first by commenting here before starting to work on it.
While submitting a PR, request a review from @nihal-rao
Doubts and clarifications are welcome.
Happy Coding!
Description
Implement any regression model to predict the self noise generated by an airfoil using various features provided.Target output is sound level in decibels.
The dataset can be found here
The given features are:
1.Frequency, in Hertzs. 2.Angle of attack, in degrees. 3.Chord length, in meters. 4.Free-stream velocity, in meters per second. 5.Suction side displacement thickness, in meters.
Details
Issue requirements / progress
Resources
airfoil_noise_starter_code.ipynb
is present in/machineLearning/33
Directory Structure
Add your solution file to 'machineLearning/33' folder. The path for your solution file should look like this:
/machineLearning/33/<your_solution_file>
Note
Please claim the issue first by commenting here before starting to work on it. While submitting a PR, request a review from @nihal-rao Doubts and clarifications are welcome. Happy Coding!