ACOUSTIC CONTROL OF FREE JET MIXING.

J. Lepicovsky; K. K. Ahuja; W. H. Brown; Philip John Morris

ACOUSTIC CONTROL OF FREE JET MIXING.

J. Lepicovsky, K. K. Ahuja, W. H. Brown, Philip John Morris

Aerospace Engineering

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Abstract

The paper reports a detailed study on the acoustic control of free jet mixing at realistic Reynolds numbers. The experimental results were obtained at Mach numbers of 0. 3 and 0. 8 and flow total temperatures up to 800 K. The Reynolds numbers ranged from 350,000 to 1,300,000. Excitation Strouhal numbers were in the range of 0. 2 to 0. 6. The experimental results are compared with predictions based on an extension of the analysis by Tam and Morris. The results showed that proper upstream tone excitation enhances mixing of unheated jets for both high-speed, high Reynolds number conditions and for low-speed conditions.

Original language	English (US)
Journal	AIAA Paper
State	Published - 1985

All Science Journal Classification (ASJC) codes

Engineering(all)

Cite this

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title = "ACOUSTIC CONTROL OF FREE JET MIXING.",

abstract = "The paper reports a detailed study on the acoustic control of free jet mixing at realistic Reynolds numbers. The experimental results were obtained at Mach numbers of 0. 3 and 0. 8 and flow total temperatures up to 800 K. The Reynolds numbers ranged from 350,000 to 1,300,000. Excitation Strouhal numbers were in the range of 0. 2 to 0. 6. The experimental results are compared with predictions based on an extension of the analysis by Tam and Morris. The results showed that proper upstream tone excitation enhances mixing of unheated jets for both high-speed, high Reynolds number conditions and for low-speed conditions.",

author = "J. Lepicovsky and Ahuja, {K. K.} and Brown, {W. H.} and Morris, {Philip John}",

year = "1985",

language = "English (US)",

journal = "AIAA Paper",

issn = "0146-3705",

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TY - JOUR

T1 - ACOUSTIC CONTROL OF FREE JET MIXING.

AU - Lepicovsky, J.

AU - Ahuja, K. K.

AU - Brown, W. H.

AU - Morris, Philip John

PY - 1985

Y1 - 1985

N2 - The paper reports a detailed study on the acoustic control of free jet mixing at realistic Reynolds numbers. The experimental results were obtained at Mach numbers of 0. 3 and 0. 8 and flow total temperatures up to 800 K. The Reynolds numbers ranged from 350,000 to 1,300,000. Excitation Strouhal numbers were in the range of 0. 2 to 0. 6. The experimental results are compared with predictions based on an extension of the analysis by Tam and Morris. The results showed that proper upstream tone excitation enhances mixing of unheated jets for both high-speed, high Reynolds number conditions and for low-speed conditions.

AB - The paper reports a detailed study on the acoustic control of free jet mixing at realistic Reynolds numbers. The experimental results were obtained at Mach numbers of 0. 3 and 0. 8 and flow total temperatures up to 800 K. The Reynolds numbers ranged from 350,000 to 1,300,000. Excitation Strouhal numbers were in the range of 0. 2 to 0. 6. The experimental results are compared with predictions based on an extension of the analysis by Tam and Morris. The results showed that proper upstream tone excitation enhances mixing of unheated jets for both high-speed, high Reynolds number conditions and for low-speed conditions.

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M3 - Article

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

ACOUSTIC CONTROL OF FREE JET MIXING.

Abstract

All Science Journal Classification (ASJC) codes

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