1. A novel preliminary design method for intermediate compressor/turbine ducts;Jinguang;Aerosp. Sci. Technol.,2021
2. Research on dynamic modeling and performance analysis of helicopter turboshaft engine's start-up process;Hanlin;Aerosp. Sci. Technol.,2020
3. The design and validation of over/under turbine-based combined cycle inlet;Huacheng;Aerosp. Sci. Technol.,2020
4. A three-dimensional body-force model for nacelle-fan systems under inlet distortions;Yinbo;Aerosp. Sci. Technol.,2020
5. Equivalent model for an axial compressor used for aero engines based on 1D and 3D analytical models and performance data;Sangjo;Aerosp. Sci. Technol.,2022