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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
1

Dynamics of laboratory models of the wind-driven ocean circulation

Kiss, Andrew Elek, Andrew.Kiss@anu.edu.au January 2001 (has links)
This thesis presents a numerical exploration of the dynamics governing rotating flow driven by a surface stress in the " sliced cylinder " model of Pedlosky & Greenspan (1967) and Beardsley (1969), and its close relative, the " sliced cone " model introduced by Griffiths & Veronis (1997). The sliced cylinder model simulates the barotropic wind-driven circulation in a circular basin with vertical sidewalls, using a depth gradient to mimic the effects of a gradient in Coriolis parameter. In the sliced cone the vertical sidewalls are replaced by an azimuthally uniform slope around the perimeter of the basin to simulate a continental slope. Since these models can be implemented in the laboratory, their dynamics can be explored by a complementary interplay of analysis and numerical and laboratory experiments. ¶ In this thesis a derivation is presented of a generalised quasigeostrophic formulation which is valid for linear and moderately nonlinear barotropic flows over large-amplitude topography on an f-plane, yet retains the simplicity and conservation properties of the standard quasigeostrophic vorticity equation (which is valid only for small depth variations). This formulation is implemented in a numerical model based on a code developed by Page (1982) and Becker & Page (1990). ¶ The accuracy of the formulation and its implementation are confirmed by detailed comparisons with the laboratory sliced cylinder and sliced cone results of Griffiths (Griffiths & Kiss, 1999) and Griffiths & Veronis (1997), respectively. The numerical model is then used to provide insight into the dynamics responsible for the observed laboratory flows. In the linear limit the numerical model reveals shortcomings in the sliced cone analysis by Griffiths & Veronis (1998) in the region where the slope and interior join, and shows that the potential vorticity is dissipated in an extended region at the bottom of the slope rather than a localised region at the east as suggested by Griffiths & Veronis (1997, 1998). Welander's thermal analogy (Welander, 1968) is used to explain the linear circulation pattern, and demonstrates that the broadly distributed potential vorticity dissipation is due to the closure of geostrophic contours in this geometry. ¶ The numerical results also provide insight into features of the flow at finite Rossby number. It is demonstrated that separation of the western boundary current in the sliced cylinder is closely associated with a " crisis " due to excessive potential vorticity dissipation in the viscous sublayer, rather than insufficient dissipation in the outer western boundary current as suggested by Holland & Lin (1975) and Pedlosky (1987). The stability boundaries in both models are refined using the numerical results, clarifying in particular the way in which the western boundary current instability in the sliced cone disappears at large Rossby and/or Ekman number. A flow regime is also revealed in the sliced cylinder in which the boundary current separates without reversed flow, consistent with the potential vorticity " crisis " mechanism. In addition the location of the stability boundary is determined as a function of the aspect ratio of the sliced cylinder, which demonstrates that the flow is stabilised in narrow basins such as those used by Beardsley (1969, 1972, 1973) and Becker & Page (1990) relative to the much wider basin used by Griffiths & Kiss (1999). ¶ Laboratory studies of the sliced cone by Griffiths & Veronis (1997) showed that the flow became unstable only under anticyclonic forcing. It is shown in this thesis that the contrast between flow under cyclonic and anticyclonic forcing is due to the combined effects of the relative vorticity and topography in determining the shape of the potential vorticity contours. The vorticity at the bottom of the sidewall smooths out the potential vorticity contours under cyclonic forcing, but distorts them into highly contorted shapes under anticyclonic forcing. In addition, the flow is dominated by inertial boundary layers under cyclonic forcing and by standing Rossby waves under anticyclonic forcing due to the differing flow direction relative to the direction of Rossby wave phase propagation. The changes to the potential vorticity structure under strong cyclonic forcing reduce the potential vorticity changes experienced by fluid columns, and the flow approaches a steady free inertial circulation. In contrast, the complexity of the flow structure under anticyclonic forcing results in strong potential vorticity changes and also leads to barotropic instability under strong forcing. ¶ The numerical results indicate that the instabilities in both models arise through supercritical Hopf bifurcations. The two types of instability observed by Griffiths & Veronis (1997) in the sliced cone are shown to be related to the western boundary current instability and " interior instability " identified by Meacham & Berloff (1997). The western boundary current instability is trapped at the western side of the interior because its northward phase speed exceeds that of the fastest interior Rossby wave with the same meridional wavenumber, as discussed by Ierley & Young (1991). ¶ Numerical experiments with different lateral boundary conditions are also undertaken. These show that the flow in the sliced cylinder is dramatically altered when the free-slip boundary condition is used instead of the no-slip condition, as expected from the work of Blandford (1971). There is no separated jet, because the flow cannot experience a potential vorticity " crisis " with this boundary condition, so the western boundary current overshoots and enters the interior from the east. In contrast, the flow in the sliced cone is identical whether no-slip, free-slip or super-slip boundary conditions are applied to the horizontal flow at the top of the sloping sidewall, except in the immediate vicinity of this region. This insensitivity results from the extremely strong topographic steering near the edge of the basin due to the vanishing depth, which demands a balance between wind forcing and Ekman pumping on the upper slope, regardless of the lateral boundary condition. The sensitivity to the lateral boundary condition is related to the importance of lateral friction in the global vorticity balance. The integrated vorticity must vanish under the no-slip condition, so in the sliced cylinder the overall vorticity budget is dominated by lateral viscosity and Ekman friction is negligible. Under the free-slip condition the Ekman friction assumes a dominant role in the dissipation, leading to a dramatic change in the flow structure. In contrast, the much larger depth variation in the sliced cone leads to a global vorticity balance in which Ekman friction is always dominant, regardless of the boundary condition.
2

Film flow over solid substrates : the effect of fluid rheology and substrate geometry and the prediction of formation of gas inclusions / Επικάλυψη στέρεης επιφάνειας με υμένα ρευστού : επίδραση της ρεολογίας του ρευστού και της μορφολογίας του υποστρώματος και πρόβλεψη δημιουργίας εγκλεισμάτων αέρα

Παυλίδης, Μιχαήλ 12 April 2010 (has links)
Surface coating is widely used in microelectronic industry to produce thin films over surfaces with uneven topography. Such processes are used in fabricating integrated circuits, storage devices, such as magnetic disks, memory devices and optical disks as well as for manufacturing adhesives, magnetic tapes, magazines which can produce thicker films over patterns of similar depth and width at higher speeds. Other applications of film flow over uneven surfaces come from specific designs of surfaces of heat-exchangers and the surfaces of various structured packings used to improve heat and mass transfer operations. The one-dimensional, gravity-driven film-flow of a linear or exponential PTT liquid, flowing either on the outer or on the inner surface of a vertical cylinder or over a planar wall is analyzed. Numerical solution of the governing equations is generally possible. Analytical solutions are derived only for: (i) linear PTT model in cylindrical and planar geometries in the absence of solvent and the affinity parameter set at zero; (ii) linear or exponential PTT model in a planar geometry in the absence of solvent and the affinity parameter the affinity parameter obtains nonzero values; (iii) exponential PTT model in planar geometry in the absence of solvent and the affinity parameter set at zero. Then, the two-dimensional, steady flow of a viscoelastic film over a periodic topography under the action of a body force is studied. It is examined the interplay of elastic, viscous, inertia and capillary forces on the film thickness and planarization efficiency over steep topographical changes of the substrate. The code is validated by verifying that in isolated topographies the periodicity conditions result in fully developed viscoelastic film flow at the inflow/outflow boundaries and that its predictions for Newtonian fluids over 2D topography under creeping flow conditions coincide with those of previous works. Finally, the steady film-flow of a Newtonian fluid has been studied over a trench examining the various types of inclusions that can be formed. It can be distinguished three possible flow configurations when (a) the triple contact points are ‘pinned’ at the lips of the cavity, (b) the triple contact points are at the left side and the bottom of the cavity so that the cavity is not filled with liquid only around its left concave corner and (c) the two triple contact points are at the two sides of the cavity so that its bottom remains empty. / Η μελέτη ρευστών υμένων κατέχει σημαντική θέση στη σύγχρονη επιστήμη και τεχνολογία και συναντάται ευρύτατα σε βιομηχανικές διεργασίες (π.χ. κατασκευή ηλεκτρονικών εξαρτημάτων όπως είναι μικροεπεξεργαστές, ολοκληρωμένα κυκλώματα και συσκευές μνήμης, κατασκευή ψηφιακών αποθηκευτικών μέσων όπως μαγνητικοί δίσκοι, δισκέτες, κασέτες και οπτικοί δίσκοι, διεργασίες φωτολιθογραφικής επικάλυψης και εκτύπωσης όπως επικαλυπτικές ουσίες, μαγνητικές ταινίες και περιοδικά κ.α.). Επιπλέον, οι ρευστοί υμένες χρησιμοποιούνται για την βελτιστοποίηση διεργασιών μεταφοράς θερμότητας και μάζας (εναλλάκτες θερμότητας). Πρώτα αναλύεται η μονοδιάστατη ροή λόγω βαρύτητας ενός υμένα ιξωδοελαστικού ρευστού που ακολουθεί το καταστατικό μοντέλο Phan-Thien and Tanner (PTT) σε γραμμική ή εκθετική μορφή. Το ρευστό ρέει είτε στην εξωτερική είτε στην εσωτερική επιφάνεια ενός κατακόρυφου κυλίνδρου ή σε επίπεδο τοίχωμα. Η αριθμητική επίλυση των διεπουσών εξισώσεων είναι πάντοτε δυνατή. Αναλυτικές εκφράσεις εξάγονται μόνο για (i) γραμμικό μοντέλο PTT σε κυλινδρικές και επίπεδες γεωμετρίες απουσία διαλύτη και η παράμετρος συγγένειας είναι μηδενική, (ii) γραμμικό ή εκθετικό μοντέλο PTT σε επίπεδη γεωμετρία απουσία διαλύτη με μη μηδενική παράμετρο συγγένειας και (iii) εκθετικό μοντέλο PTT σε επίπεδη γεωμετρία απουσία διαλύτη και με μηδενική παράμετρο συγγένειας. Στη συνέχεια μελετάται η δισδιάστατη μόνιμη ροή ενός ιξωδοελαστικού υμένα κατά μήκος περιοδικής τοπογραφίας υπό την επίδραση είτε της βαρύτητας είτε της φυγοκέντρου δύναμης. Εξετάζεται τόσο η επίδραση των ιξωδοελαστικών ιδιοτήτων υπό συνθήκες έρπουσας ροής όσο και των τριχοειδών και αδρανειακών δυνάμεων καθώς και της γεωμετρίας του υποστρώματος στο πάχος του υμένα και στη δυνατότητα εξομάλυνσής του παρά τις απότομες αλλαγές του υποστρώματος. Ο κώδικας ελέγχθηκε μέσω της σύγκρισης των προβλέψεών του με προηγούμενες εργασίες που αφορούν σε Νευτωνικά και σε ιξωδοελαστικά ρευστά. Τέλος, εξετάζεται η δισδιάστατη μόνιμη ροή ενός Νευτωνικού υμένα πάνω από παρόμοια μεταβαλλόμενο υπόστρωμα, ενώ επιτρέπεται να σχηματίζονται εγκλείσματα αέρα μεταξύ του υμένα και του υποστρώματος. Διακρίνονται οι εξής δυνατότητες σχηματισμού εγκλεισμάτων αέρα ανάλογα με τη θέση της κάτω επιφάνειας του υμένα: (α) εμφανίζονται σταθερά σημεία επαφής στις άνω (κυρτές) γωνίες του υποστρώματος, (β) σχηματίζεται έγκλεισμα γύρω από την πρώτη κοίλη γωνία του υποστρώματος και (γ) εμφανίζονται δύο τριπλά σημεία επαφής με τις παράπλευρες επιφάνειες του υποστρώματος.

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