In this paper, a high speed Turbojet-Scramjet combined engine is constructed, and the engine performance calculation is completed. The mission of long range strike is set as target aircraft’s main mission. A corresponding flight profile was found. Aircraft/power integrated design model was developed, which used to evaluate the aircraft performance of finishing the mission. The calculation results show that the combined engine can work in the Ma 0-6 and 0-25km airspace. The target aircraft assembled the engine can complete the high-altitude and high-speed long-range strike mission.
Performance Calculation and Integrated Mission Assessment of High Speed Turbojet-Scramjet Combined Engine
2018-07-01
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Conference paper
Electronic Resource
English
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