Analysis of particle laden flows around a jet vane in a solid rocket motor

H. H. Cho, B. G. Kirn, M. S. Yu, Y. W. Nam, K. Y. Hwang, J. C. Bae

Research output: Contribution to conferencePaper

Abstract

The flow in the nozzle of a solid propellant rocket is characterized by a two-phase flow including A12O3 particles generated by combustion. The present study was conducted for the numerical analysis on the particle laden flow around a jet vane device which is installed at the end of the nozzle for the thrust vector control. The particle accretion rate on the vane surface was obtained as the fundamental information of the vane erosion analysis. Primarily, the analysis of the flow was carried out around a simple two dimensional jet vane model and then an actual three dimensional jet vane to understand the two phase flow phenomena. The vane turning angle and the particle size were considered as the main parameters changed from 0° to 20° and from 0.5μm to 20μm, respectively.

Original languageEnglish
Publication statusPublished - 2001 Dec 1
Event37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States
Duration: 2001 Jul 82001 Jul 11

Other

Other37th Joint Propulsion Conference and Exhibit 2001
CountryUnited States
CitySalt Lake City, UT
Period01/7/801/7/11

Fingerprint

Rocket engines
Two phase flow
Nozzles
Solid propellants
Rockets
Numerical analysis
Erosion
Particle size

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Cho, H. H., Kirn, B. G., Yu, M. S., Nam, Y. W., Hwang, K. Y., & Bae, J. C. (2001). Analysis of particle laden flows around a jet vane in a solid rocket motor. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.
Cho, H. H. ; Kirn, B. G. ; Yu, M. S. ; Nam, Y. W. ; Hwang, K. Y. ; Bae, J. C. / Analysis of particle laden flows around a jet vane in a solid rocket motor. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.
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abstract = "The flow in the nozzle of a solid propellant rocket is characterized by a two-phase flow including A12O3 particles generated by combustion. The present study was conducted for the numerical analysis on the particle laden flow around a jet vane device which is installed at the end of the nozzle for the thrust vector control. The particle accretion rate on the vane surface was obtained as the fundamental information of the vane erosion analysis. Primarily, the analysis of the flow was carried out around a simple two dimensional jet vane model and then an actual three dimensional jet vane to understand the two phase flow phenomena. The vane turning angle and the particle size were considered as the main parameters changed from 0° to 20° and from 0.5μm to 20μm, respectively.",
author = "Cho, {H. H.} and Kirn, {B. G.} and Yu, {M. S.} and Nam, {Y. W.} and Hwang, {K. Y.} and Bae, {J. C.}",
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note = "37th Joint Propulsion Conference and Exhibit 2001 ; Conference date: 08-07-2001 Through 11-07-2001",

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Cho, HH, Kirn, BG, Yu, MS, Nam, YW, Hwang, KY & Bae, JC 2001, 'Analysis of particle laden flows around a jet vane in a solid rocket motor' Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States, 01/7/8 - 01/7/11, .

Analysis of particle laden flows around a jet vane in a solid rocket motor. / Cho, H. H.; Kirn, B. G.; Yu, M. S.; Nam, Y. W.; Hwang, K. Y.; Bae, J. C.

2001. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.

Research output: Contribution to conferencePaper

TY - CONF

T1 - Analysis of particle laden flows around a jet vane in a solid rocket motor

AU - Cho, H. H.

AU - Kirn, B. G.

AU - Yu, M. S.

AU - Nam, Y. W.

AU - Hwang, K. Y.

AU - Bae, J. C.

PY - 2001/12/1

Y1 - 2001/12/1

N2 - The flow in the nozzle of a solid propellant rocket is characterized by a two-phase flow including A12O3 particles generated by combustion. The present study was conducted for the numerical analysis on the particle laden flow around a jet vane device which is installed at the end of the nozzle for the thrust vector control. The particle accretion rate on the vane surface was obtained as the fundamental information of the vane erosion analysis. Primarily, the analysis of the flow was carried out around a simple two dimensional jet vane model and then an actual three dimensional jet vane to understand the two phase flow phenomena. The vane turning angle and the particle size were considered as the main parameters changed from 0° to 20° and from 0.5μm to 20μm, respectively.

AB - The flow in the nozzle of a solid propellant rocket is characterized by a two-phase flow including A12O3 particles generated by combustion. The present study was conducted for the numerical analysis on the particle laden flow around a jet vane device which is installed at the end of the nozzle for the thrust vector control. The particle accretion rate on the vane surface was obtained as the fundamental information of the vane erosion analysis. Primarily, the analysis of the flow was carried out around a simple two dimensional jet vane model and then an actual three dimensional jet vane to understand the two phase flow phenomena. The vane turning angle and the particle size were considered as the main parameters changed from 0° to 20° and from 0.5μm to 20μm, respectively.

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M3 - Paper

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Cho HH, Kirn BG, Yu MS, Nam YW, Hwang KY, Bae JC. Analysis of particle laden flows around a jet vane in a solid rocket motor. 2001. Paper presented at 37th Joint Propulsion Conference and Exhibit 2001, Salt Lake City, UT, United States.