1982
DOI: 10.1093/qjmam/35.1.69
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Asymptotic Analysis of the Orr-Sommerfeld Problem for Boundary-Layer Flows

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Cited by 7 publications
(4 citation statements)
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“…We determined the minimum critical Reynolds number Re,,, and the corresponding critical values of aCrit and cCrit. These were Recrit = 46095, a,,,, = 0.1592, cCrit = 0.1564, and compare very favourably with those found by Lakin & Reid (1982) We performed a numerical solution of the full system of differential equations and boundary conditions (6.27)-(6.33) by a similar method to that described in $5. Our results are displayed in table 2 for the model lead alloy data given in table 1 but with Sc = 5.…”
Section: )supporting
confidence: 71%
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“…We determined the minimum critical Reynolds number Re,,, and the corresponding critical values of aCrit and cCrit. These were Recrit = 46095, a,,,, = 0.1592, cCrit = 0.1564, and compare very favourably with those found by Lakin & Reid (1982) We performed a numerical solution of the full system of differential equations and boundary conditions (6.27)-(6.33) by a similar method to that described in $5. Our results are displayed in table 2 for the model lead alloy data given in table 1 but with Sc = 5.…”
Section: )supporting
confidence: 71%
“…This confirms the above analysis that indicates that the shear flow mode of instability is unaffected by the presence of the freezing interface for high Schmidt numbers. The quantitative disparity between the asymptotic results and the numerical solution of the governing equations can be attributed to the neglect of the D3 operation in the approximations to the Orr-Sommerfeld equation, as was remarked by Lakin & Reid (1982).…”
Section: )mentioning
confidence: 97%
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“…On the other hand, high resolution is required in the thin active region of the perturbations, making it impractical to integrate much further from the interface than the outer limit of the active regions. The imposition of an artificial top or floor is known to yield spurious modes in the resulting eigenfunction spectrum (Lakin & Grosch 1982). Therefore we have truncated the velocity distribution in the air by choosing simple G .…”
Section: Model Of the Shear Flowmentioning
confidence: 99%