This project explores the use of supervised learning and deep learning models to predict Shock-Train Leading Edge (STLE) locations in hypersonic vehicles using sparse pressure sensor data.
π All code is implemented in Jupyter notebooks and based on experimental aerodynamic data.
Given time-series pressure sensor readings from hypersonic wind tunnel experiments, the goal is to accurately predict the location of STLE β a key aerodynamic event that influences vehicle stability at high speeds.
- Built baseline and advanced supervised learning models:
- Linear Regression
- Random Forest
- Support Vector Machines (SVM)
- Feed-forward Neural Network
- Recurrent Neural Network
- Engineered time-series features to denoise pressure signals and improve model accuracy
- Trained a deep neural network using only 7 of 37 total runs and evaluated on >900K test observations
- π Improved RΒ² from 0.79 to 0.89
- π§ͺ DNN generalized well to unseen test conditions, despite limited training set size
