Combustion flow in ejecting mode of strutjet engine (II) Effects of secondary combustion and configuration

Sheng Hong Huang; Hong Qing He; Guo Qiang He

Combustion flow in ejecting mode of strutjet engine (II) Effects of secondary combustion and configuration

Sheng Hong Huang
, Hong Qing He
, Guo Qiang He

航天学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

3-D turbulent flows with and without secondary combustion of two configurations of Strutjet RBCC in ejecting mode were investigated. The effects of secondary combustion and configurations on ejecting flow in static sea-level and zero Mach conditions were analyzed in detail. The conclusion is that the velocity, total temperature, total pressure and secondary air mass flow rate are determined by both effects of configuration and secondary combustion, but the mixing degree between primary and secondary flow is mainly controlled by configuration, and thus the performance of RBCC.

源语言	英语
页（从-至）	259-264
页数	6
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	24
期	3
出版状态	已出版 - 6月 2003

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abstract = "3-D turbulent flows with and without secondary combustion of two configurations of Strutjet RBCC in ejecting mode were investigated. The effects of secondary combustion and configurations on ejecting flow in static sea-level and zero Mach conditions were analyzed in detail. The conclusion is that the velocity, total temperature, total pressure and secondary air mass flow rate are determined by both effects of configuration and secondary combustion, but the mixing degree between primary and secondary flow is mainly controlled by configuration, and thus the performance of RBCC.",

keywords = "Ejection flow field, Ejector ramjet engine, Rocket based combined cycle",

author = "Huang, \{Sheng Hong\} and He, \{Hong Qing\} and He, \{Guo Qiang\}",

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AU - Huang, Sheng Hong

AU - He, Hong Qing

AU - He, Guo Qiang

PY - 2003/6

Y1 - 2003/6

N2 - 3-D turbulent flows with and without secondary combustion of two configurations of Strutjet RBCC in ejecting mode were investigated. The effects of secondary combustion and configurations on ejecting flow in static sea-level and zero Mach conditions were analyzed in detail. The conclusion is that the velocity, total temperature, total pressure and secondary air mass flow rate are determined by both effects of configuration and secondary combustion, but the mixing degree between primary and secondary flow is mainly controlled by configuration, and thus the performance of RBCC.

AB - 3-D turbulent flows with and without secondary combustion of two configurations of Strutjet RBCC in ejecting mode were investigated. The effects of secondary combustion and configurations on ejecting flow in static sea-level and zero Mach conditions were analyzed in detail. The conclusion is that the velocity, total temperature, total pressure and secondary air mass flow rate are determined by both effects of configuration and secondary combustion, but the mixing degree between primary and secondary flow is mainly controlled by configuration, and thus the performance of RBCC.

KW - Ejection flow field

KW - Ejector ramjet engine

KW - Rocket based combined cycle

UR - https://www.scopus.com/pages/publications/0141456392

M3 - 文章

AN - SCOPUS:0141456392

SN - 1001-4055

VL - 24

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EP - 264

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 3

ER -

Combustion flow in ejecting mode of strutjet engine (II) Effects of secondary combustion and configuration

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