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.


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    Title :

    Performance Calculation and Integrated Mission Assessment of High Speed Turbojet-Scramjet Combined Engine


    Contributors:
    Rui-yuan, KANG (author) / Yu-chun, CHEN (author) / Yuan, GAO (author)


    Publication date :

    2018-07-01


    Size :

    7324353 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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