MEASUREMENTS OF MASS TRANSFER COEFFICIENT AND EFFECTIVENESS IN THE RECOVERY REGION OF A FILM-COOLED SURFACE.

W. P. Webster, Savas Yavuzkurt

Research output: Contribution to journalArticle

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Abstract

Mass transfer coefficients and film cooling effectiveness are measured downstream of a single row of holes inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. The mass transfer coefficients (based on the difference between the free stream and the surface concentrations) are measured using a naphthalene sublimation technique. Experiments are carried out in a subsonic, zero pressure gradient turbulent boundary layer, under isothermal conditions with three blowing ratios (U//j/U// infinity ): 0. 4, 0. 8, and 1. 2. The data is collected in a region 7 to 80 jet diameters downstream of the injection location. From the data on mass transfer coefficients and effectiveness obtained under the same flow conditions a general mass transfer equation is derived. This paper presents extensive data and discussions.

Original languageEnglish (US)
Journal[No source information available]
StatePublished - 1986

Fingerprint

Mass transfer
Recovery
Boundary layer flow
Sublimation
Naphthalene
Blow molding
Pressure gradient
Boundary layers
Cooling
Experiments

All Science Journal Classification (ASJC) codes

  • Mechanical Engineering

Cite this

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title = "MEASUREMENTS OF MASS TRANSFER COEFFICIENT AND EFFECTIVENESS IN THE RECOVERY REGION OF A FILM-COOLED SURFACE.",
abstract = "Mass transfer coefficients and film cooling effectiveness are measured downstream of a single row of holes inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. The mass transfer coefficients (based on the difference between the free stream and the surface concentrations) are measured using a naphthalene sublimation technique. Experiments are carried out in a subsonic, zero pressure gradient turbulent boundary layer, under isothermal conditions with three blowing ratios (U//j/U// infinity ): 0. 4, 0. 8, and 1. 2. The data is collected in a region 7 to 80 jet diameters downstream of the injection location. From the data on mass transfer coefficients and effectiveness obtained under the same flow conditions a general mass transfer equation is derived. This paper presents extensive data and discussions.",
author = "Webster, {W. P.} and Savas Yavuzkurt",
year = "1986",
language = "English (US)",
journal = "[No source information available]",
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}

MEASUREMENTS OF MASS TRANSFER COEFFICIENT AND EFFECTIVENESS IN THE RECOVERY REGION OF A FILM-COOLED SURFACE. / Webster, W. P.; Yavuzkurt, Savas.

In: [No source information available], 1986.

Research output: Contribution to journalArticle

TY - JOUR

T1 - MEASUREMENTS OF MASS TRANSFER COEFFICIENT AND EFFECTIVENESS IN THE RECOVERY REGION OF A FILM-COOLED SURFACE.

AU - Webster, W. P.

AU - Yavuzkurt, Savas

PY - 1986

Y1 - 1986

N2 - Mass transfer coefficients and film cooling effectiveness are measured downstream of a single row of holes inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. The mass transfer coefficients (based on the difference between the free stream and the surface concentrations) are measured using a naphthalene sublimation technique. Experiments are carried out in a subsonic, zero pressure gradient turbulent boundary layer, under isothermal conditions with three blowing ratios (U//j/U// infinity ): 0. 4, 0. 8, and 1. 2. The data is collected in a region 7 to 80 jet diameters downstream of the injection location. From the data on mass transfer coefficients and effectiveness obtained under the same flow conditions a general mass transfer equation is derived. This paper presents extensive data and discussions.

AB - Mass transfer coefficients and film cooling effectiveness are measured downstream of a single row of holes inclined 30 degrees with the surface and inline with the main turbulent boundary layer flow. The mass transfer coefficients (based on the difference between the free stream and the surface concentrations) are measured using a naphthalene sublimation technique. Experiments are carried out in a subsonic, zero pressure gradient turbulent boundary layer, under isothermal conditions with three blowing ratios (U//j/U// infinity ): 0. 4, 0. 8, and 1. 2. The data is collected in a region 7 to 80 jet diameters downstream of the injection location. From the data on mass transfer coefficients and effectiveness obtained under the same flow conditions a general mass transfer equation is derived. This paper presents extensive data and discussions.

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