In Part I of this thesis, steady and time-dependent, natural-convection similarity flows with mass transfer are discussed. Similarity flows for natural convection on families of two-dimensional bodies with closed lower ends are enumerated, when both a temperature distribution and a suction velocity distribution are prescribed at the body surface. For steady similarity flow on a heated vertical flat plate, with mass transfer at the surface, a numerical procedure is introduced for determining the velocity and temperature profiles. These results are presented in Figs. 2 and 3. Other similarity flows may be found by the same method. A simplification, valid for “strong” suction, is discussed. An extension of Mangler's transformation [1948] is given which reduces the equations governing axisymmetric flow to those for two-dimensional flow in steady natural convection. In Part II non-linear resonant instability in parallel shear flows is discussed. A.D.D.Craik's (see Usher and Craik [I]) modified version of Bateman's [1956] variational formulation for viscous flows is employed to derive the second-order interaction equations governing the temporal evolution of a resonant wave triad in a sheer flow. (An extension of Craik's variational formulation to free surface flows is presented but is not required in the subsequent analysis for the resonance problem). This problem was treated previously using a ‘direct' approach (employing the Navier-Stokes equations) by Craik [1971]. The major advantage of the present method over the ‘direct' method is the substantial reduction in algebraic complexity. Also, a justification of the validity of Craik's previous analysis is given. For this same resonance problem, third-order interaction equations are derived by the *direct* method since, to this order of approximation, little advantage is to be gained from the variational formulation. The resonance theory is thereby developed to the same order of approximation as the non-resonant third-order theory of Stuart [1960, 1962]. An asymptotic analysis for large Reynolds numbers reveals that the magnitudes of the third-order interaction coefficients – like certain of those at second-order – are remarkably large. Such results lead to a discussion of the regions of validity of the perturbation analysis. Also some light is shed on the roles played by resonance and three-dimensionality in the non-linear instability of shear flows.

Thesis (Ph. D.)--University of Texas at Austin, 1999. / Vita. Includes bibliographical references (leaves 206-219). Available also in a digital version from Dissertation Abstracts.

This dissertation presents a technique for the solution of incompressible equivalents to planar steady subsonic potential flows. Riemannian geometric formalism is used to develop a gauge transformation of the length measure followed by a curvilinear coordinate transformation to map a subsonic flow into a canonical Laplacian flow with the same boundary conditions. The method represents the generalization of the methods of Prandtl-Glauert and Karman-Tsien and gives exact results in the sense that the inverse mapping produces the subsonic full potential solution over the original airfoil, up to numerical accuracy. The motivation for this research was provided by the analogy between linear potential flow and the special theory of relativity that emerges from the invariance of the wave equation under Lorentz transformations. Whereas elements of the special theory can be invoked for linear and global compressibility effects, the question posed in this work is whether other techniques from relativity theory could be used for effects that are nonlinear and local. This line of thought leads to a transformation leveraging Riemannian geometric methods common to the general theory of relativity. The dissertation presents the theory and a numerical method for practical solutions of equivalent incompressible flows over arbitrary profiles. The numerical method employs an iterative approach involving the solution of the incompressible flow with a panel method and the solution of the coordinate mapping to the canonical flow with a finite difference approach. This method is demonstrated for flow over a circular cylinder and over a NACA 0012 profile. Results are validated with subcritical full potential test cases available in the literature. Two areas of applicability of the method have been identified. The first is airfoil inverse design leveraging incompressible flow knowledge and empirical data for the potential field effects on boundary layer transition and separation. The second is aerodynamic testing using distorted models.

Thesis (Ph. D.)--University of Washington, 2002. / Vita. Includes bibliographical references (p. 178-185).

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Orientador: Jun Takahashi / Tese (doutorado) - Universidade Estadual de Campinas, Instituto de Fisica Gleb Wataghin / Made available in DSpace on 2018-08-23T16:49:52Z (GMT). No. of bitstreams: 1 Souza_RafaelDerradide_D.pdf: 5902855 bytes, checksum: ef026256d77f665d1d9d346c08ad7ec8 (MD5) Previous issue date: 2013 / Resumo: Nas colisões nucleares relativísticas, devido ao comportamento coletivo do sistema, é esperado que a anisotropia espacial inicial da região de uperposição entre os núcleos incidentes seja convertida em uma anisotropia final na distribuição de momento das partículas produzidas. Em particular, o coeficiente de fluxo elíptico, dado pelo segundo harmônico (v2) da decomposição de Fourier da distribuição azimutal das partículas finais produzidas, é um observável sensível à anisotropia geométrica inicial. Neste trabalho, estudamos o comportamento do coeficiente v2 obtido a partir de eventos gerados com o código de evolução hidrodinâmica NeXSPheRIO simulando colisões Au+Au a (SNN)1/2 = 200 GeV. O NeXSPheRIO permite o controle da condição inicial, da evolução hidrodinâmica e gera as partículas finais como em um evento real. Portanto, foi possível aplicar as mesmas técnicas de análise de dados utilizadas experimentalmente. Estudamos os efeitos de flutuações na condição inicial no observável v2 e testamos alguns observáveis experimentais propostos que seriam sensíveis a estas flutuações. Como os observáveis também são sensíveis a outros tipos de correlações, geralmente chamadas de non-flow, e considerando que a maior contribuição pode vir de jatos de partículas gerados nessas colisões, estudamos os efeitos de jatos nesses observáveis. Construímos um modelo simplificado de duas componentes a partir da superposição de eventos NeXSPheRIO, com eventos de colisões p+p produzidos pelo gerador de eventos Pythia. Resultados deste modelo descrevem melhor a dependência de v2 com o momento transversal quando comparados com dados experimentais. Determinamos também que, ao contrário do que se esperava, os observáveis sensíveis à flutuação na condição inicial são pouco afetados pela inclusão dos jatos. Este resultado sugere que os efeitos de non-flow, como considerados aqui, são desprezíveis nas medidas de flutuações de v2, indicando que os resultados obtidos pelos experimentos sejam dominados pelas flutuações da condição inicial / Abstract: Due to the collective behavior of the system created in relativistic nuclear collisions, it is expected that the initial spatial anisotropy of the overlap region between the two incoming nuclei converts into an anisotropy of the momentum distribution of the outgoing particles. In particular, the elliptic flow coefficient, which is given by the second harmonic (v2) of the Fourier decomposition of the final particle azimuthal distribution, is an observable sensitive to the initial geometric anisotropy. In this work, we studied the behavior of the elliptic flow coefficient obtained from events generated using the hydrodynamic-based code NeXSPheRIO for Au+Au collisions at (SNN)1/2= 200 GeV. The NeXSPheRIO code allows the control of the initial condition, the hydrodynamic evolution and produces the outgoing particles just like in a real event. Therefore, it was possible to apply the same data analysis techniques used experimentally. We studied the effects of initial condition fluctuations on flow observables and tested some experimental observables thought to be sensitive to the fluctuations. Since these observables are also sensitive to other types of correlations, usually referred to as non-flow, and considering that the major contribution to them may come from jets of particles generated in the collision, we also studied the effects of jets on these observables. A simplified two-component model was built by superimposing events produced with the NeXSPheRIO code and p+p collision events produced with the Pythia event generator. Results from our model present a better description of the ?2 dependence with transverse momentum when compared to experimental data. Also, opposite to what was expected, the observables sensitive to the fluctuations are not much sensitive to the inclusion of jets. This result may suggest that the contribution of non-flow, as considered here, is negligible in the observed flow fluctuations measurement, which indicates that the values observed in the experiments are mainly dominated by fluctuations from the initial condition / Doutorado / Física / Doutor em Ciências