TY - CONF
T1 - Turbulent mixing in plane and axisymmetric shear layers
AU - Morris, Philip J.
AU - Giridharan, M. G.
AU - Viswanathan, K.
N1 - Funding Information:
This work was supported by the Office of Naval Research and the Air Force Office of Scientific Research under grant N00014-88-K-0242. The technical monitors are Drs. Spiro Lekoudis and Julian Tishkoff.
Publisher Copyright:
© 1990 American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 1990
Y1 - 1990
N2 - This paper considers two problems associated with turbulent mixing in high speed shear layers. In the first we extend a previous model by the authors for two-dimensional shear layers to consider axisymmetric shear layers. The model assumes that large scale coherent structures dominate the mixing process in free shear layers. These large structures are modeled locally as instability waves. Calculations are made for the development of the axisymmetric shear layer as a function of freestream Mach numbers, velocity and density ratios. The calculations for the axisymmetric case are compared with the two-dimensional calculations and experimental results. In the second part of the paper we consider the effect of confining walls on the development of a two-dimensional shear layer. The effects of changing the wall locations in both the spanwise and normal directions are considered. The various classes of instability waves that exist are examined. The relationship between the span-wise confined and unconfined shear layers is examined. It is shown that the growth rates of instabilities may be maximized by the correct choice of duct width to height ratio.
AB - This paper considers two problems associated with turbulent mixing in high speed shear layers. In the first we extend a previous model by the authors for two-dimensional shear layers to consider axisymmetric shear layers. The model assumes that large scale coherent structures dominate the mixing process in free shear layers. These large structures are modeled locally as instability waves. Calculations are made for the development of the axisymmetric shear layer as a function of freestream Mach numbers, velocity and density ratios. The calculations for the axisymmetric case are compared with the two-dimensional calculations and experimental results. In the second part of the paper we consider the effect of confining walls on the development of a two-dimensional shear layer. The effects of changing the wall locations in both the spanwise and normal directions are considered. The various classes of instability waves that exist are examined. The relationship between the span-wise confined and unconfined shear layers is examined. It is shown that the growth rates of instabilities may be maximized by the correct choice of duct width to height ratio.
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M3 - Paper
AN - SCOPUS:85003674308
T2 - 28th Aerospace Sciences Meeting, 1990
Y2 - 8 January 1990 through 11 January 1990
ER -