@inproceedings{7dea7bff754a420380c4e7b212d5a4d8,
title = "An optimization method for non-augmented supersonic cruise performance of turbofan engine",
abstract = "Based on the component maps based gas turbine engine simulation model, the engine steady-state performance calculation model is established. Based on the model, the non-augmented supersonic cruise performance of the fourth-generation engine is studied. The effect of different rotational speed of the high-pressure rotor design values and different throttle ratios on engine velocity characteristics is analyzed. The effect of adjusting the throat area of the tail nozzle on the engine velocity characteristics is analyzed. Finally, the non-augmented supersonic cruise performance of the fourth-generation engine has been optimized.",
keywords = "Non-augmented supersonic cruise, Tail nozzle throat area adjustment, Turbofan engine, Velocity characteristics",
author = "Ma, \{Xin Yue\} and Gou, \{Lin Feng\} and Tian Tan",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 ; Conference date: 22-07-2019 Through 25-07-2019",
year = "2019",
month = jul,
doi = "10.1109/ICMAE.2019.8880993",
language = "英语",
series = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "122--127",
booktitle = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
}