Regression analysis on the selection of hybrid rocket engine with suitable nano–additives
摘要
The continuous pursuit of enhanced performance, environmental compatibility, and cost efficiency in hybrid rocket engines (HREs) has led to the exploration of nano-additives as energetic performance enhancers. This research investigates the regression behaviour and performance prediction of hybrid rocket engines enhanced with nano-additives using an Adaptive Gaussian Process Regression with Principal Component Reduction (Adaptive GPR-PCR) framework. Seven additives- Aluminium (Al), Boron (B), Sodium Borohydride (NaBH4), Potassium Borohydride (KBH4), Potassium Nitrate (KNO3), Lithium Aluminium Hydride (LiAlH4), and Lithium Borohydride (LiBH4) -were analysed based on their thermal conductivity, decomposition enthalpy, and hydrogen yield to quantify their influence on regression rate (