About this document
Diverterless Supersonic Intake Optimization by 21103020 is a document available to read on EtoBox.
This document presents a novel design method for a diverterless supersonic intake (DSI) that integrates a bump into a curved fuselage, enhancing performance through an efficient global optimization technique. The proposed method minimizes computational load while achieving a 38.3% improvement in performance index by optimizing design parameters like bump geometry and cowl sweep angle. The study utilizes a Kriging surrogate model and genetic algorithms to identify optimal designs, demonstrating significant a
- Author
- 21103020
- Language
- EN