EFFECTS OF INJECTION ON CONDENSATION ON A FILM-COOLED SURFACE.

William Phil Webster; Savash Yavuzkurt

EFFECTS OF INJECTION ON CONDENSATION ON A FILM-COOLED SURFACE.

William Phil Webster
, Savash Yavuzkurt

Institute for Computational and Data Sciences (ICDS)

Research output: Contribution to journal › Conference article › peer-review

Abstract

Gas turbine blades have previously been shown to corrode due to condensation of sulfide vapor on a cooled blade surface. In the present investigation, water vapor was condensed on a film cooled surface, simulating the condensation of sulfide vapor on a turbine blade. The injection section consisted of one row of holes (inner diameter of 1. 0 cm) inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. Experiments were carried out in a subsonic, zero pressure gradient, turbulent boundary layer with free stream velocities of 10. 5, 15. 75, and 21. 0 m/sec.

Original language	English (US)
Journal	American Society of Mechanical Engineers (Paper)
State	Published - Jan 1 1987

All Science Journal Classification (ASJC) codes

Mechanical Engineering

Cite this

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title = "EFFECTS OF INJECTION ON CONDENSATION ON A FILM-COOLED SURFACE.",

abstract = "Gas turbine blades have previously been shown to corrode due to condensation of sulfide vapor on a cooled blade surface. In the present investigation, water vapor was condensed on a film cooled surface, simulating the condensation of sulfide vapor on a turbine blade. The injection section consisted of one row of holes (inner diameter of 1. 0 cm) inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. Experiments were carried out in a subsonic, zero pressure gradient, turbulent boundary layer with free stream velocities of 10. 5, 15. 75, and 21. 0 m/sec.",

author = "Webster, \{William Phil\} and Savash Yavuzkurt",

year = "1987",

month = jan,

day = "1",

language = "English (US)",

journal = "American Society of Mechanical Engineers (Paper)",

issn = "0402-1215",

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T1 - EFFECTS OF INJECTION ON CONDENSATION ON A FILM-COOLED SURFACE.

AU - Webster, William Phil

AU - Yavuzkurt, Savash

PY - 1987/1/1

Y1 - 1987/1/1

N2 - Gas turbine blades have previously been shown to corrode due to condensation of sulfide vapor on a cooled blade surface. In the present investigation, water vapor was condensed on a film cooled surface, simulating the condensation of sulfide vapor on a turbine blade. The injection section consisted of one row of holes (inner diameter of 1. 0 cm) inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. Experiments were carried out in a subsonic, zero pressure gradient, turbulent boundary layer with free stream velocities of 10. 5, 15. 75, and 21. 0 m/sec.

AB - Gas turbine blades have previously been shown to corrode due to condensation of sulfide vapor on a cooled blade surface. In the present investigation, water vapor was condensed on a film cooled surface, simulating the condensation of sulfide vapor on a turbine blade. The injection section consisted of one row of holes (inner diameter of 1. 0 cm) inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. Experiments were carried out in a subsonic, zero pressure gradient, turbulent boundary layer with free stream velocities of 10. 5, 15. 75, and 21. 0 m/sec.

UR - https://www.scopus.com/pages/publications/0023172074

UR - https://www.scopus.com/pages/publications/0023172074#tab=citedBy

M3 - Conference article

AN - SCOPUS:0023172074

SN - 0402-1215

JO - American Society of Mechanical Engineers (Paper)

JF - American Society of Mechanical Engineers (Paper)

ER -

EFFECTS OF INJECTION ON CONDENSATION ON A FILM-COOLED SURFACE.

Abstract

All Science Journal Classification (ASJC) codes

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