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

School of Power and Energy

Northwestern Polytechnical University Xian

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	122-127
Number of pages	6
ISBN (Electronic)	9781728155357
DOIs	https://doi.org/10.1109/ICMAE.2019.8880993
State	Published - Jul 2019
Event	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, Belgium Duration: 22 Jul 2019 → 25 Jul 2019

Publication series

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

Conference

Conference	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Country/Territory	Belgium
City	Brussels
Period	22/07/19 → 25/07/19

Keywords

Non-augmented supersonic cruise
Tail nozzle throat area adjustment
Turbofan engine
Velocity characteristics

Access to Document

10.1109/ICMAE.2019.8880993

Cite this

Ma, X. Y., Gou, L. F., & Tan, T. (2019). An optimization method for non-augmented supersonic cruise performance of turbofan engine. In 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 (pp. 122-127). Article 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. pp. 122-127 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

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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.",

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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. in 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., pp. 122-127, 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019, Brussels, Belgium, 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. p. 122-127 8880993 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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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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PB - Institute of Electrical and Electronics Engineers Inc.

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Ma XY, Gou LF, Tan T. An optimization method for non-augmented supersonic cruise performance of turbofan engine. In 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc. 2019. p. 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

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