한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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- Pages.117-121
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- 2003
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- 1975-342X(pISSN)
이상 브레이튼 사이클에서의 램 제트 추진기관 성능의 기본 특성
Performance Characters of the Ramjet Based on Ideal Brayton Cycle
초록
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.
키워드