EFFECTS OF PHYSICAL PROPERTIES AND LOCATION IN THE PLUME ON MEAN DROPLET DIAMETER FOR TRANSVERSE LIQUID INJECTION IN A SUPERSONIC AIR STREAM.

A. S. Nejad; J. A. Schetz

doi:10.2514/6.1981-188

EFFECTS OF PHYSICAL PROPERTIES AND LOCATION IN THE PLUME ON MEAN DROPLET DIAMETER FOR TRANSVERSE LIQUID INJECTION IN A SUPERSONIC AIR STREAM.

A. S. Nejad^*, J. A. Schetz

^*Corresponding author for this work

King Fahd University of Petroleum & Minerals

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

Abstract

The mean droplet diameter in the spray resulting from transverse injection of liquid jets into a supersonic airstream was investigated in detail by the use of the Diffractively Scattered Light Method. The effects of viscosity, surface tension, jet/free airstream dynamic pressure ratio, injection diameter and location in the plume on the mean droplet diameter were determined. All tests were performed at M// infinity equals 3. 0 with P//o equals 4. 2 atm. and T//Q equals 300 degree K. The injectants used were water and various solutions of glycerine and ethanol in water to produce wide variations in viscosity and surface tension. The important results are summarized.

Original language	English
Journal	AIAA Paper
DOIs	https://doi.org/10.2514/6.1981-188
State	Published - 1981

ASJC Scopus subject areas

General Engineering

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title = "EFFECTS OF PHYSICAL PROPERTIES AND LOCATION IN THE PLUME ON MEAN DROPLET DIAMETER FOR TRANSVERSE LIQUID INJECTION IN A SUPERSONIC AIR STREAM.",

abstract = "The mean droplet diameter in the spray resulting from transverse injection of liquid jets into a supersonic airstream was investigated in detail by the use of the Diffractively Scattered Light Method. The effects of viscosity, surface tension, jet/free airstream dynamic pressure ratio, injection diameter and location in the plume on the mean droplet diameter were determined. All tests were performed at M// infinity equals 3. 0 with P//o equals 4. 2 atm. and T//Q equals 300 degree K. The injectants used were water and various solutions of glycerine and ethanol in water to produce wide variations in viscosity and surface tension. The important results are summarized.",

author = "Nejad, \{A. S.\} and Schetz, \{J. A.\}",

year = "1981",

doi = "10.2514/6.1981-188",

language = "English",

journal = "AIAA Paper",

issn = "0146-3705",

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AU - Nejad, A. S.

AU - Schetz, J. A.

PY - 1981

Y1 - 1981

N2 - The mean droplet diameter in the spray resulting from transverse injection of liquid jets into a supersonic airstream was investigated in detail by the use of the Diffractively Scattered Light Method. The effects of viscosity, surface tension, jet/free airstream dynamic pressure ratio, injection diameter and location in the plume on the mean droplet diameter were determined. All tests were performed at M// infinity equals 3. 0 with P//o equals 4. 2 atm. and T//Q equals 300 degree K. The injectants used were water and various solutions of glycerine and ethanol in water to produce wide variations in viscosity and surface tension. The important results are summarized.

AB - The mean droplet diameter in the spray resulting from transverse injection of liquid jets into a supersonic airstream was investigated in detail by the use of the Diffractively Scattered Light Method. The effects of viscosity, surface tension, jet/free airstream dynamic pressure ratio, injection diameter and location in the plume on the mean droplet diameter were determined. All tests were performed at M// infinity equals 3. 0 with P//o equals 4. 2 atm. and T//Q equals 300 degree K. The injectants used were water and various solutions of glycerine and ethanol in water to produce wide variations in viscosity and surface tension. The important results are summarized.

UR - https://www.scopus.com/pages/publications/85088620918

U2 - 10.2514/6.1981-188

DO - 10.2514/6.1981-188

M3 - Conference article

AN - SCOPUS:85088620918

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

EFFECTS OF PHYSICAL PROPERTIES AND LOCATION IN THE PLUME ON MEAN DROPLET DIAMETER FOR TRANSVERSE LIQUID INJECTION IN A SUPERSONIC AIR STREAM.

Abstract

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