Test and analysis of thrust from pulsed detonation engine

Liming He; Tongmo Xu; Chuanjun Yan; Linquan Wang; Wei Fan; Hengren Lei

Test and analysis of thrust from pulsed detonation engine

Liming He, Tongmo Xu, Chuanjun Yan, Linquan Wang, Wei Fan, Hengren Lei

Xi'an Jiaotong University

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

Quantitative determination and analysis are made to study the thrust produced by a pulsed detonation engine. Particular emphases are placed on the influence of excess air coefficient of mixture, detonating frequency and detonation frequency on the thrust. Performance data are obtained, and they are in good agreement with the calculated results.

源语言	英语
页（从-至）	18-21
页数	4
期刊	Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University
卷	32
期	10
出版状态	已出版 - 1998
已对外发布	是

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title = "Test and analysis of thrust from pulsed detonation engine",

abstract = "Quantitative determination and analysis are made to study the thrust produced by a pulsed detonation engine. Particular emphases are placed on the influence of excess air coefficient of mixture, detonating frequency and detonation frequency on the thrust. Performance data are obtained, and they are in good agreement with the calculated results.",

author = "Liming He and Tongmo Xu and Chuanjun Yan and Linquan Wang and Wei Fan and Hengren Lei",

year = "1998",

language = "英语",

volume = "32",

pages = "18--21",

journal = "Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University",

issn = "0253-987X",

publisher = "Xi'an Jiaotong University",

number = "10",

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TY - JOUR

T1 - Test and analysis of thrust from pulsed detonation engine

AU - He, Liming

AU - Xu, Tongmo

AU - Yan, Chuanjun

AU - Wang, Linquan

AU - Fan, Wei

AU - Lei, Hengren

PY - 1998

Y1 - 1998

N2 - Quantitative determination and analysis are made to study the thrust produced by a pulsed detonation engine. Particular emphases are placed on the influence of excess air coefficient of mixture, detonating frequency and detonation frequency on the thrust. Performance data are obtained, and they are in good agreement with the calculated results.

AB - Quantitative determination and analysis are made to study the thrust produced by a pulsed detonation engine. Particular emphases are placed on the influence of excess air coefficient of mixture, detonating frequency and detonation frequency on the thrust. Performance data are obtained, and they are in good agreement with the calculated results.

UR - http://www.scopus.com/inward/record.url?scp=0032275663&partnerID=8YFLogxK

M3 - 文章

AN - SCOPUS:0032275663

SN - 0253-987X

VL - 32

SP - 18

EP - 21

JO - Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University

JF - Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University

IS - 10

ER -

Test and analysis of thrust from pulsed detonation engine

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