Performance Characters of the Ramjet Based on Ideal Brayton Cycle

이상 브레이튼 사이클에서의 램 제트 추진기관 성능의 기본 특성

In order to investigate the performance characters of the ramjet propulsion, at the first step, in this paper Ideal Brayton cycle is adopted. In the Ideal Ramjet cycle some of the Parameters are independent of the heat input, for example thermal efficiency but in the Ideal Brayton cycle, Mach number and the entry temperature of the combustion chamber are important variables with the heat input.