An optimization method for non-augmented supersonic cruise performance of turbofan engine

Xin Yue Ma; Lin Feng Gou; Tian Tan

doi:10.1109/ICMAE.2019.8880993

An optimization method for non-augmented supersonic cruise performance of turbofan engine

Xin Yue Ma, Lin Feng Gou, Tian Tan

动力与能源学院

Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

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.

源语言	英语
主期刊名	2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
出版商	Institute of Electrical and Electronics Engineers Inc.
页	122-127
页数	6
ISBN（电子版）	9781728155357
DOI	https://doi.org/10.1109/ICMAE.2019.8880993
出版状态	已出版 - 7月 2019
活动	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, 比利时期限: 22 7月 2019 → 25 7月 2019

出版系列

姓名	2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

会议

会议	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
国家/地区	比利时
市	Brussels
时期	22/07/19 → 25/07/19

访问文件

10.1109/ICMAE.2019.8880993

其它文件与链接

链接到 Scopus 的出版物

引用此

Ma, X. Y., Gou, L. F., & Tan, T. (2019). An optimization method for non-augmented supersonic cruise performance of turbofan engine. 在 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 (页码 122-127). 文章 8880993 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMAE.2019.8880993

Ma, Xin Yue ; Gou, Lin Feng ; Tan, Tian. / An optimization method for non-augmented supersonic cruise performance of turbofan engine. 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 122-127 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

@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",

}

Ma, XY, Gou, LF & Tan, T 2019, An optimization method for non-augmented supersonic cruise performance of turbofan engine. 在 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019., 8880993, 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019, Institute of Electrical and Electronics Engineers Inc., 页码 122-127, 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019, Brussels, 比利时, 22/07/19. https://doi.org/10.1109/ICMAE.2019.8880993

An optimization method for non-augmented supersonic cruise performance of turbofan engine. / Ma, Xin Yue; Gou, Lin Feng; Tan, Tian.
2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 页码 122-127 8880993 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - An optimization method for non-augmented supersonic cruise performance of turbofan engine

AU - Ma, Xin Yue

AU - Gou, Lin Feng

AU - Tan, Tian

PY - 2019/7

Y1 - 2019/7

N2 - 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.

AB - 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.

KW - Non-augmented supersonic cruise

KW - Tail nozzle throat area adjustment

KW - Turbofan engine

KW - Velocity characteristics

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U2 - 10.1109/ICMAE.2019.8880993

DO - 10.1109/ICMAE.2019.8880993

M3 - 会议稿件

AN - SCOPUS:85074838650

T3 - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

SP - 122

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BT - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

Y2 - 22 July 2019 through 25 July 2019

ER -

Ma XY, Gou LF, Tan T. An optimization method for non-augmented supersonic cruise performance of turbofan engine. 在 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 页码 122-127. 8880993. (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019). doi: 10.1109/ICMAE.2019.8880993

An optimization method for non-augmented supersonic cruise performance of turbofan engine

摘要

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