Optimization of Orifice Geometry for Cross-flow Mixing in a Cylindrical Duct

Optimization of Orifice Geometry for Cross-flow Mixing in a Cylindrical Duct PDF Author: W. A. Sowa
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Optimization of Orifice Geometry for Cross-flow Mixing in a Cylindrical Duct

Optimization of Orifice Geometry for Cross-flow Mixing in a Cylindrical Duct PDF Author: W. A. Sowa
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Optimization of Orifice Geometry for Cross-Flow Mixing in a Cylindrical Duct

Optimization of Orifice Geometry for Cross-Flow Mixing in a Cylindrical Duct PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 82

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Optimization of Orifice Geometry for Cross-Flow Mixing in a Cylindrical Duct

Optimization of Orifice Geometry for Cross-Flow Mixing in a Cylindrical Duct PDF Author: National Aeronaut Administration (Nasa)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722682514
Category :
Languages : en
Pages : 84

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Mixing of gaseous jets in a cross-flow has significant applications in engineering, one example of which is the dilution zone of a gas turbine combustor. Despite years of study, the design of the jet injection in combustors is largely based on practical experience. The emergence of NO(x) regulations for stationary gas turbines and the anticipation of aero-engine regulations requires an improved understanding of jet mixing as new combustor concepts are introduced. For example, the success of the staged combustor to reduce the emission of NO(x) is almost entirely dependent upon the rapid and complete dilution of the rich zone products within the mixing section. It is these mixing challenges to which the present study is directed. A series of experiments was undertaken to delineate the optimal mixer orifice geometry. A cross-flow to core-flow momentum-flux ratio of 40 and a mass flow ratio of 2.5 were selected as representative of a conventional design. An experimental test matrix was designed around three variables: the number of orifices, the orifice length-to- width ratio, and the orifice angle. A regression analysis was performed on the data to arrive at an interpolating equation that predicted the mixing performance of orifice geometry combinations within the range of the test matrix parameters. Results indicate that the best mixing orifice geometry tested involves eight orifices with a long-to-short side aspect ratio of 3.5 at a twenty-three degree inclination from the center-line of the mixing section. Kroll, J. T. and Sowa, W. A. and Samuelsen, G. S. Glenn Research Center...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 542

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Optimization of Circular Orifice Jets Mixing Into a Heated Cross Flow in a Cylindrical Duct

Optimization of Circular Orifice Jets Mixing Into a Heated Cross Flow in a Cylindrical Duct PDF Author: J. T. Kroll
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Optimization of Jet Mixing Into a Rich, Reacting Crossflow

Optimization of Jet Mixing Into a Rich, Reacting Crossflow PDF Author: M. Y. Leong
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 752

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

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Crossflow Mixing of Noncircular Jets

Crossflow Mixing of Noncircular Jets PDF Author: D. S. Liscinsky
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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CFD Assessment of Orifice Aspect Ratio and Mass Flow Ratio on Jet Mixing in Rectangular Ducts

CFD Assessment of Orifice Aspect Ratio and Mass Flow Ratio on Jet Mixing in Rectangular Ducts PDF Author: D. B. Bain
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 38

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