Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow

Alexander Yarin, A. Arkadyev, P. Bar-Yoseph

Research output: Contribution to journalArticle

Abstract

Deposition of particles onto a turbine blade in cascade inclined at some angle to the flow at infinity is considered. The submicron particles are thermophoretically deposited onto the blade surface, whereas supermicron particles strike it inertially. A coating at the foil surface is accumulated due to the thermophoretical deposition and polished as a result of supermicron particle strikes. The competition of these two processes does not lead (generally as regards the flow around the foil) to the emergence of steady-state continuous coating at the blade surface. However, some slowly growing coating islands may be obtained and used to protect the blade. The effects of various flow and blade parameters on the coating growth are studied.

Original languageEnglish
Pages (from-to)243-248
Number of pages6
JournalInternational Journal of Turbo and Jet Engines
Volume11
Issue number2-3
DOIs
Publication statusPublished - 1994
Externally publishedYes

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Turbomachine blades
Flow of gases
Turbines
Coatings
Metal foil
Cascades (fluid mechanics)

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow. / Yarin, Alexander; Arkadyev, A.; Bar-Yoseph, P.

In: International Journal of Turbo and Jet Engines, Vol. 11, No. 2-3, 1994, p. 243-248.

Research output: Contribution to journalArticle

Yarin, Alexander ; Arkadyev, A. ; Bar-Yoseph, P. / Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow. In: International Journal of Turbo and Jet Engines. 1994 ; Vol. 11, No. 2-3. pp. 243-248.
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