This paper develops an integrated high speed vehicle/combined power performance analysis model, using the mission requirements of hypersonic vehicles in near space as a traction. The ability of this power to perform typical tasks was assessed using a rotating detonation combined cycle engine. The effect of different wing loading, different take-off weights and different climb modes on the performance of the vehicle was also studied, and the important performance parameters of the high-speed vehicle and engine in the flight profile were obtained. The results of the study show that the rotating detonation combined cycle engine is suitable for large range missions, based on the turbojet and turbofan rotating detonation combined cycle engine range increase of 42.3% and 33.5% respectively compared to TBCC.As the wing loading increases, the cruising distance tends to increase and then decrease; as the gross take-off weight increases, the combined effect of increased fuel mass and reduced thrust-to-weight ratio results in an increasing and then decreasing range. The lower the dynamic pressure, the longer the climbing time and the distance climbed increases significantly, the higher the dynamic pressure, the shorter the climbing time and the less fuel is consumed during the climb.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Integrated Analysis of Rotating Detonation Combined Cycle Engines


    Beteiligte:
    Zhao, Zhennan (Autor:in) / Jia, Linyuan (Autor:in) / Zhang, Yining (Autor:in) / Kong, Fanqi (Autor:in)


    Erscheinungsdatum :

    18.07.2023


    Format / Umfang :

    633151 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Thermodynamic Power Cycle Analysis in Actively Cooled Rotating Detonation Rocket Engines

    Cobb, Garrett R. / Durkee, Kaito J. / Burr, Jason R. et al. | AIAA | 2025


    Investigation of Limit Cycle Oscillation Persistence Within Rotating Detonation Engines

    Johnson, Kristyn / Weber, Justin / Ferguson, Donald H. et al. | AIAA | 2025


    Progress of continuously rotating detonation engines

    Zhou, Rui / Wu, Dan / Wang, Jianping | British Library Online Contents | 2016


    Combustion Characteristics in Rotating Detonation Engines

    Yuhui Wang / Wenyou Qiao / JialingLe | DOAJ | 2021

    Freier Zugriff

    Asymptotic Dynamics of Rotating Detonation Engines

    Kickliter, Trevor / Acharya, Vishal S. / Lieuwen, Tim et al. | AIAA | 2025