Spreadsheet Calculations for Jets in Crossflow From Single and Opposed Rows With Alternating Hole Sizes

Author:

Holdeman J. D.1,Clisset J. R.2,Moder J. P.3

Affiliation:

1. National Aeronautics and Space Administration, Glenn Research Center, Cleveland, OH 44135

2. University of Florida, Gainesville, FL 32611

3. Combustion Branch, Propulsion Systems Division, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, OH 44135

Abstract

The primary purpose of this study was to show the expected results for cases of single and opposed rows of jets from alternating large and small round holes. Previous publications demonstrated that the NASA empirical model gave results that were an excellent representation of mean experimental scalar results and that the model could confidently be used to investigate configurations for which results have not been published in the open literature. Calculations for cases of opposed rows of jets that would overpenetrate slightly in an inline configuration showed that better mixing was attained when one row was shifted to make a staggered configuration so that a small hole was opposite from a larger one. However, the result was no better than for an optimum inline configuration with all the holes of the same size. Staggering the rows does not make much difference in an optimum inline configuration. For all cases investigated, the dimensionless variance of the mixture fraction decreased significantly with increasing downstream distance, but, at a given downstream location, the variation between cases was small.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference12 articles.

1. Mixing of Multiple Jets With a Confined Subsonic Crossflow;Holdeman;Prog. Energy Combust. Sci.

2. Mixing of Multiple Jets With a Confined Subsonic Crossflow: Part I—Cylindrical Ducts;Holdeman;ASME J. Eng. Gas Turbines Power

3. Mixing of Multiple Jets With a Confined Crossflow: Part II—Opposed Rows of Orifices in Rectangular Ducts;Holdeman;ASME J. Eng. Gas Turbines Power

4. Holdeman, J. D., Smith, T. D., Clisset, J. R., and Lear, W. E., 2005, “A Spreadsheet for the Mixing of a Row of Jets With a Confined Crossflow,” NASA Report No. NASA/TM-2005-213137.

5. Holdeman, J. D., Clisset, J. R., Moder, J. P., and Lear, W. E., 2006, “On the Mixing of Single and Opposed Rows of Jets With a Confined Crossflow,” NASA Report No. NASA/TM-2006-214226.

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