Research on the jet influence on the mechanical launcher of various ignition height

Weidong He; Yi Jiang; Yanli Ma

doi:10.1007/978-3-642-31507-7_11

Research on the jet influence on the mechanical launcher of various ignition height

Weidong He^*, Yi Jiang, Yanli Ma

^*Corresponding author for this work

School of Aerospace Engineering

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

Abstract

In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.

Original language	English
Title of host publication	Advances in Mechanical and Electronic Engineering
Pages	57-63
Number of pages	7
Edition	VOL. 1
DOIs	https://doi.org/10.1007/978-3-642-31507-7_11
Publication status	Published - 2012
Event	2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012 - Hefei, China Duration: 23 Jun 2012 → 24 Jun 2012

Publication series

Name	Lecture Notes in Electrical Engineering
Number	VOL. 1
Volume	176 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012
Country/Territory	China
City	Hefei
Period	23/06/12 → 24/06/12

Keywords

ignition height
launching mechanical equipment
numerical simulation
rocket plume

Access to Document

10.1007/978-3-642-31507-7_11

Cite this

@inproceedings{46ed6fc0c9414288b6d8737300ba464b,

title = "Research on the jet influence on the mechanical launcher of various ignition height",

abstract = "In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.",

keywords = "ignition height, launching mechanical equipment, numerical simulation, rocket plume",

author = "Weidong He and Yi Jiang and Yanli Ma",

year = "2012",

doi = "10.1007/978-3-642-31507-7_11",

language = "English",

isbn = "9783642315060",

series = "Lecture Notes in Electrical Engineering",

number = "VOL. 1",

pages = "57--63",

booktitle = "Advances in Mechanical and Electronic Engineering",

edition = "VOL. 1",

note = "2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012 ; Conference date: 23-06-2012 Through 24-06-2012",

}

He, W, Jiang, Y & Ma, Y 2012, Research on the jet influence on the mechanical launcher of various ignition height. in Advances in Mechanical and Electronic Engineering. VOL. 1 edn, Lecture Notes in Electrical Engineering, no. VOL. 1, vol. 176 LNEE, pp. 57-63, 2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012, Hefei, China, 23/06/12. https://doi.org/10.1007/978-3-642-31507-7_11

Research on the jet influence on the mechanical launcher of various ignition height. / He, Weidong; Jiang, Yi; Ma, Yanli.
Advances in Mechanical and Electronic Engineering. VOL. 1. ed. 2012. p. 57-63 (Lecture Notes in Electrical Engineering; Vol. 176 LNEE, No. VOL. 1).

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

TY - GEN

T1 - Research on the jet influence on the mechanical launcher of various ignition height

AU - He, Weidong

AU - Jiang, Yi

AU - Ma, Yanli

PY - 2012

Y1 - 2012

N2 - In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.

AB - In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.

KW - ignition height

KW - launching mechanical equipment

KW - numerical simulation

KW - rocket plume

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U2 - 10.1007/978-3-642-31507-7_11

DO - 10.1007/978-3-642-31507-7_11

M3 - Conference contribution

AN - SCOPUS:84867052402

SN - 9783642315060

T3 - Lecture Notes in Electrical Engineering

SP - 57

EP - 63

BT - Advances in Mechanical and Electronic Engineering

T2 - 2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012

Y2 - 23 June 2012 through 24 June 2012

ER -

Research on the jet influence on the mechanical launcher of various ignition height

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Keywords

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