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Predicting the stability of a compressible periodic parallel jet flowIt is known that mixing enhancement in compressible free shear layer flows with high convective Mach numbers is difficult. One design strategy to get around this is to use multiple nozzles. Extrapolating this design concept in a one dimensional manner, one arrives at an array of parallel rectangular nozzles where the smaller dimension is omega and the longer dimension, b, is taken to be infinite. In this paper, the feasibility of predicting the stability of this type of compressible periodic parallel jet flow is discussed. The problem is treated using Floquet-Bloch theory. Numerical solutions to this eigenvalue problem are presented. For the case presented, the interjet spacing, s, was selected so that s/omega =2.23. Typical plots of the eigenvalue and stability curves are presented. Results obtained for a range of convective Mach numbers from 3 to 5 show growth rates omega(sub i)=kc(sub i)/2 range from 0.25 to 0.29. These results indicate that coherent two-dimensional structures can occur without difficulty in multiple parallel periodic jet nozzles and that shear layer mixing should occur with this type of nozzle design.
Document ID
19960027989
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miles, Jeffrey H.
(NASA Lewis Research Center Cleveland,OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-107206
E-10205
NAS 1.15:107206
Meeting Information
Meeting: 1996 Fluids Engineering Conference
Location: San Diego, CA
Country: United States
Start Date: July 7, 1996
End Date: July 11, 1996
Sponsors: American Society of Mechanical Engineers
Accession Number
96N29108
Funding Number(s)
PROJECT: RTOP 537-05-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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