关键词: 涡轮风扇发动机;冲压式喷气发动机;航空航天飞机;组合式发动机;设计;研究

Abstract: The ATR/RJ combined engine performance at constant dynamic pressure is analyzed.Based on the data, the transition condition is considered and calculated. Also, the static temperature, static pressure in combustor, airflow rate and thrust under the condition of various dynamic pressure were compared respectively.All the performance parameters presented in the paper are useful for the design of the airturborocket/ramjet combined engine.

Key words: Fanjet engine;Ramjet engine;Composite engine;Aerospace craft;Design;Research