Analysis of particle laden flow and heat transfer in cascade and rocket nozzle

H. H. Cho, W. S. Kim, M. S. Yu, J. C. Bae

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

This paper presents results for the calculation of particle trajectories in a cascade and a rocket nozzle using a Lagrangian method. When the floating particles collide to the components, the component surface is damaged severely. The surface erosion rate is strongly dependent on a particle size, a particle impact angle and a surface material. For a compressor cascade, the particle impact rate increases proportionally with the flow inlet angle and the erosion rate on the pressure side surface of blade are related to the surface or coating materials. For a solid rocket nozzle, the particle free zone in the nozzle divergent section increases quickly with increasing particle size and the maximum heat transfer density occurs at the starting region of nozzle convergent section. The Al2O3 droplet breaks up around the nozzle throat due to the high velocity difference between the droplet and gas stream, resulting in the big change of particle free zone.

Original languageEnglish
Pages (from-to)233-240
Number of pages8
JournalAnnals of the New York Academy of Sciences
Volume934
Publication statusPublished - 2001 Jan 1

Fingerprint

Rocket nozzles
Particle Size
Hot Temperature
Heat transfer
Pharynx
Nozzles
Gases
Erosion
Pressure
Particle size
Inlet flow
Compressors
Trajectories
Heat
Particle
Coatings

All Science Journal Classification (ASJC) codes

  • Neuroscience(all)
  • Biochemistry, Genetics and Molecular Biology(all)
  • History and Philosophy of Science

Cite this

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abstract = "This paper presents results for the calculation of particle trajectories in a cascade and a rocket nozzle using a Lagrangian method. When the floating particles collide to the components, the component surface is damaged severely. The surface erosion rate is strongly dependent on a particle size, a particle impact angle and a surface material. For a compressor cascade, the particle impact rate increases proportionally with the flow inlet angle and the erosion rate on the pressure side surface of blade are related to the surface or coating materials. For a solid rocket nozzle, the particle free zone in the nozzle divergent section increases quickly with increasing particle size and the maximum heat transfer density occurs at the starting region of nozzle convergent section. The Al2O3 droplet breaks up around the nozzle throat due to the high velocity difference between the droplet and gas stream, resulting in the big change of particle free zone.",
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Analysis of particle laden flow and heat transfer in cascade and rocket nozzle. / Cho, H. H.; Kim, W. S.; Yu, M. S.; Bae, J. C.

In: Annals of the New York Academy of Sciences, Vol. 934, 01.01.2001, p. 233-240.

Research output: Contribution to journalArticle

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