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Direct simulation for the instability and breakup of laminar liquid jetsA direct numerical simulation method is described for predicting the deformation of laminar liquid jets. In the present nonlinear direct simulation, the convective term, which has been discarded in past linear analyses by Rayleigh and others, is included in the hydrodynamic equations. It is shown that only by maintaining full complexity of the nonlinear surface tension term accurate drop formation can be predicted. The continuity and momentum equations in the transient form are integrated on an adaptive grid, conforming the jet and surface wave shape. The equations, which are parabolic in time and elliptic in space, are solved by a TVD scheme with characteristic flux splitting. The results of the present work are discussed and compared with available measurements and other analyses. The comparison shows that among the predictions, the current 1-D direct simulation results agree best with the experimental data. Furthermore, the computer time requirements are much (an order of magnitude) smaller than those of previously reported multidimensional analyses.
Document ID
19900053554
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chuech, S. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Przekwas, A. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Yang, H. Q.
(CFD Research Corp. Huntsville, AL, United States)
Gross, K. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 90-2066
Accession Number
90A40609
Funding Number(s)
CONTRACT_GRANT: NAS8-38425
Distribution Limits
Public
Copyright
Other

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