Paper Contents
Abstract
This study investigates the performance of a supersonic intake system for a ramjet engine, focusing on the impact of a elliptical bleeding process. By manipulating airflow and pressure conditions, we analyze how bleed mechanisms enhance engine efficiency and stability during supersonic flight. Experimental tests reveal variations in thrust and fuel efficiency, highlighting the critical role of bleed air in managing shock waves and improving combustion dynamics. Results indicate optimal bleed configurations that maximize performance across various flight conditions. This research contributes to the design of advanced ramjet systems, offering insights into balancing intake performance with engine operability in high-speed environments.
Copyright
Copyright © 2025 UMAMAHESH MOYYI. This is an open access article distributed under the Creative Commons Attribution License.
