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Supersonic Jet Noise Reduction by Coaxial Jets with Coplanar and Staggered Exits

Dosanjh, D. S. and Matambo, Thompson and Gharib, Morteza (1979) Supersonic Jet Noise Reduction by Coaxial Jets with Coplanar and Staggered Exits. American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20130913-074732862

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Abstract

Far-field noise radiated from coaxial cold underexpanded jet flows issuing from convergent two-nozzle configurations with coplanar and staggered-exits is investigated experimentally. The coaxial jets are operated in the "inverted" mode, i.e., the outer (annular) jet flow Mach number is higher than that of the inner (round) jet. Keeping all other geometrical and operating conditions the same, the exit-stagger of the inner (round) and the outer (annular) nozzles was varied. It is shown that the extent of the exit-stagger affects both the flows and the radiated noise from such coaxial underexpanded jet flows and that comparatively, the lowest noise levels are achieved when the coaxial nozzle-exits are coplanar. Moreover, the effectiveness of the co-flowing inner jet flow in reducing the noise radiated from either the annular or the coaxial underexpanded jet flows decreases noticeably as the exit-stagger is increased.


Item Type:Report or Paper (Report)
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/6.1979-672DOIReport
http://arc.aiaa.org/doi/abs/10.2514/6.1979-672PublisherReport
Additional Information:© 1979 American Institute of Aeronautics and Astronautics, Inc. Our thanks to Mrs. K. Curtice for the typing of this paper.
Group:GALCIT
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper79-0672
Record Number:CaltechAUTHORS:20130913-074732862
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20130913-074732862
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:41304
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:17 Sep 2013 20:10
Last Modified:30 Sep 2016 17:35

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