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- J. Fluid Mech. (2001), vol. 430, pp. 267282. Printed in the United Kingdom c 2001 Cambridge University Press
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- Journal of Computational Physics 157, 787795 (2000) doi:10.1006/jcph.1999.6382, available online at http://www.idealibrary.com on
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- J. Fluid Mech. (2008), vol. 599, pp. 309339. c 2008 Cambridge University Press doi:10.1017/S0022112007009925 Printed in the United Kingdom
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- J. Fluid Mech. (2002), vol. 455, pp. 315346. c 2002 Cambridge University Press DOI: 10.1017/S0022112001007534 Printed in the United Kingdom
- J. Fluid Mech. (1997), vol. 330, pp. 375409 Copyright c 1997 Cambridge University Press
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