Aerodynamic Noise Control Study of Nozzles with Triangular Chevrons

Article Preview

Abstract:

This paper has a small part of notion of chevron and the process that helps reducing the noise pollution. Based on the gas dynamic and geometrical parameters of a single flow jet engine one does a model of CFD data processing. In this process one observes the influence of chevrons on acoustic wave intensity produced by the jet . One studies a series of tests on triangular chevrons: immersions, the influence of the number of chevrons in order to settle the influence of the geometrical parameters on the flow and on the jet acoustics. Finally one presents the contribution of chevrons in noise pollution reduction.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

25-31

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Youn D., Jet noise suppression means, United States Patent Office, No. US3153319, oct. 20 1964, p.7.

Google Scholar

[2] Balzer, Segment mixing device having chevrons for exhaust noise reduction in jet engines, United States Patent Office, No. US6612106, sept. 2, 2003, p.4.

DOI: 10.1121/1.2857693

Google Scholar

[3] Mathews et al.,  Tabbed nozzle for jet noise suppression , United States Patent Office, No. US6314721, nov. 13, 2001,  p.8.

Google Scholar

[4] Dorin Stanciu, Termodinamica tehnica, Publishing house Bucuresti, (2004).

Google Scholar

[5] Bogdan Gherman, Virgil Stanciu, Valentin Silivestru, Comparatia unei noi solutii de motor, motorul tripluflux, cu motorul dubluflux, Aerospatial Conference, Bucharest, (2008).

Google Scholar

[6] Ansys 12 Documentation-User's Guide (2004).

Google Scholar

[7] James Bridges and Clifford A. Brown Glenn Research Center, Cleveland, Ohio, Parametric Testing of Chevrons on Single Flow Hot Jets, NASA/TM—2004-213107, September 2004, AIAA–2004–2824.

DOI: 10.2514/6.2004-2824

Google Scholar

[8] P. S. Tide and K. Srinivasan, Far-field acoustic investigation on six lobed chevron nozzles, INCAST, (2008).

Google Scholar

[9] Ronald L Balzer, U.S. Patent 6612106 B2. (2003).

Google Scholar