Numerical simulation of performance for turbine based combined cycle propulsion system

Zeng Wen Liu; Zhan Xue Wang; Yuan Hu Cai; Hui Min Ma

Numerical simulation of performance for turbine based combined cycle propulsion system

Zeng Wen Liu
, Zhan Xue Wang
, Yuan Hu Cai
, Hui Min Ma

动力与能源学院

Northwestern Polytechnical University Xian
Beijing Power Machinery Research Institute

科研成果: 期刊稿件 › 文章 › 同行评审

11 引用（Scopus）

摘要

The arrangement of turbine based combined cycle engines were investigated. Co-axial and tandem configuration was selected as a turbofan-ram combined engine. The design parameters of both turbofan engine and ramjet were laid out, and the rules were expounded to explain how to ascertain the transition point of operation mode. Based on a modular structure code, the performance characteristic of turbo-ramjet was simulated by numerical method.

源语言	英语
页（从-至）	1-4+51
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	30
期	1
出版状态	已出版 - 2月 2009

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引用此

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title = "Numerical simulation of performance for turbine based combined cycle propulsion system",

abstract = "The arrangement of turbine based combined cycle engines were investigated. Co-axial and tandem configuration was selected as a turbofan-ram combined engine. The design parameters of both turbofan engine and ramjet were laid out, and the rules were expounded to explain how to ascertain the transition point of operation mode. Based on a modular structure code, the performance characteristic of turbo-ramjet was simulated by numerical method.",

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AU - Wang, Zhan Xue

AU - Cai, Yuan Hu

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N2 - The arrangement of turbine based combined cycle engines were investigated. Co-axial and tandem configuration was selected as a turbofan-ram combined engine. The design parameters of both turbofan engine and ramjet were laid out, and the rules were expounded to explain how to ascertain the transition point of operation mode. Based on a modular structure code, the performance characteristic of turbo-ramjet was simulated by numerical method.

AB - The arrangement of turbine based combined cycle engines were investigated. Co-axial and tandem configuration was selected as a turbofan-ram combined engine. The design parameters of both turbofan engine and ramjet were laid out, and the rules were expounded to explain how to ascertain the transition point of operation mode. Based on a modular structure code, the performance characteristic of turbo-ramjet was simulated by numerical method.

KW - Numerical simulation

KW - Performance

KW - Turbine based combined cycle propulsion system

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M3 - 文章

AN - SCOPUS:62749153751

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JO - Tuijin Jishu/Journal of Propulsion Technology

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Numerical simulation of performance for turbine based combined cycle propulsion system

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