超燃冲压发动机温度及热流测量技术研究进展

Xinhang Jin; Binghe Ma; Tao Qiu; Jinjun Deng; Jian Luo

doi:10.11729/syltlx20170013

超燃冲压发动机温度及热流测量技术研究进展

Translated title of the contribution: Temperature and heat flux measurement technologies in scramjet

Xinhang Jin, Binghe Ma, Tao Qiu, Jinjun Deng, Jian Luo

School of Microelectronics

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

The accurate measurement of temperature and heat flux field in scramjet provides strong support for characterization, assessment and optimization of scramjet engine. Measurement methods are reviewed and analyzed, including sheathed and thin film sensors, and photoelectric method and radiation method.

Translated title of the contribution	Temperature and heat flux measurement technologies in scramjet
Original language	Chinese (Traditional)
Pages (from-to)	74-81
Number of pages	8
Journal	Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics
Volume	32
Issue number	2
DOIs	https://doi.org/10.11729/syltlx20170013
State	Published - 1 Apr 2018

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title = "超燃冲压发动机温度及热流测量技术研究进展",

abstract = "The accurate measurement of temperature and heat flux field in scramjet provides strong support for characterization, assessment and optimization of scramjet engine. Measurement methods are reviewed and analyzed, including sheathed and thin film sensors, and photoelectric method and radiation method.",

keywords = "Heat flux, High-temperature, Scramjet, Thin-film heat flux, Thin-film thermocouples",

author = "Xinhang Jin and Binghe Ma and Tao Qiu and Jinjun Deng and Jian Luo",

year = "2018",

month = apr,

day = "1",

doi = "10.11729/syltlx20170013",

language = "繁体中文",

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pages = "74--81",

journal = "Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics",

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T1 - 超燃冲压发动机温度及热流测量技术研究进展

AU - Jin, Xinhang

AU - Ma, Binghe

AU - Qiu, Tao

AU - Deng, Jinjun

AU - Luo, Jian

PY - 2018/4/1

Y1 - 2018/4/1

N2 - The accurate measurement of temperature and heat flux field in scramjet provides strong support for characterization, assessment and optimization of scramjet engine. Measurement methods are reviewed and analyzed, including sheathed and thin film sensors, and photoelectric method and radiation method.

AB - The accurate measurement of temperature and heat flux field in scramjet provides strong support for characterization, assessment and optimization of scramjet engine. Measurement methods are reviewed and analyzed, including sheathed and thin film sensors, and photoelectric method and radiation method.

KW - Heat flux

KW - High-temperature

KW - Scramjet

KW - Thin-film heat flux

KW - Thin-film thermocouples

UR - http://www.scopus.com/inward/record.url?scp=85059091937&partnerID=8YFLogxK

U2 - 10.11729/syltlx20170013

DO - 10.11729/syltlx20170013

M3 - 文章

AN - SCOPUS:85059091937

SN - 1672-9897

VL - 32

SP - 74

EP - 81

JO - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

JF - Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

IS - 2

ER -

超燃冲压发动机温度及热流测量技术研究进展

Abstract

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