2010
DOI: 10.1016/j.ijengsci.2010.05.001
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On the laminar boundary-layer flow over rotating spheroids

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Cited by 10 publications
(5 citation statements)
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“…Due to the complex relation between r and s for a spheroid we have not verified that equations (8a,b) can be transformed to (23a,b). Nevertheless, velocity profiles calculated by the present method compare well with those generated by Samad and Garrett (2010) in figure 9 for e = 0.3; however, for the higher eccentricity case of e = 0.7, figure 10, the agreement, while good initially, is poor at increased latitude θ. The discrepancy appears to be connected with the different mapping of the η co-ordinates used by Garrett (2010, 2014) and in the present work, as the magnitudes of the peak velocities agree closely.…”
supporting
confidence: 51%
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“…Due to the complex relation between r and s for a spheroid we have not verified that equations (8a,b) can be transformed to (23a,b). Nevertheless, velocity profiles calculated by the present method compare well with those generated by Samad and Garrett (2010) in figure 9 for e = 0.3; however, for the higher eccentricity case of e = 0.7, figure 10, the agreement, while good initially, is poor at increased latitude θ. The discrepancy appears to be connected with the different mapping of the η co-ordinates used by Garrett (2010, 2014) and in the present work, as the magnitudes of the peak velocities agree closely.…”
supporting
confidence: 51%
“…The equations for the boundary layer of a rotating prolate spheroid in still air, first investigated by Fadnis (1954), are shown here as formulated by Samad and Garrett (2010), rotating axi-symmetric body to be analysed, both with and without an axial flow. Comparisons with other published shape-specific formulations appear to confirm the validity of both the mathematical formulation and the numerical scheme employed, but there are some isolated discrepancies which remain to be resolved.…”
Section: Rotating Prolate Spheroid In Still Airmentioning
confidence: 99%
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“…(8) are nondimensional with the Reynolds number, Re = ωR 2 /ν, θ being the tangential location andδ being the normalized boundary layer thickness,δ = δ/R. Equation (8) is solved subject to the condition thatδ = 0 at θ = 0 to yield an expression for the boundary layer …”
Section: A Region A: Boundary Layer Flowmentioning
confidence: 99%