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Analysis of kinetic models and macroscopic continuum equations for rarefied gas dynamicsZheng, Yingsong 10 April 2008 (has links)
The Boltzmann equation is the basic equation to describe rarefied gas flows. Some
kinetic models with simple expressions for the collision term have been proposed to
reduce the mathematical complexity of the Boltzmann equation. All macroscopic
continuum equations can be derived from the Boltzmann equation or kinetic models
through the Chapman-Enskog method, Grad's moment method, etc.
This thesis is divided into three parts. In the first part, existing kinetic models (BGK
model, ES-BGK model, v(C) -BGK model, S model, and Liu model), and two newly
proposed v(C)-ES-BGK type kinetic models are described and compared, based on
properties that need to be satisfied for a kinetic model. In the new models a meaningful
expression for the collision frequency is used, while the important properties for a kinetic
model are retained at the same time.
In the second part of this work, the kinetic models (BGK, ES-BGK, v(C) -BGK, and
two new kinetic models) are tested numerically for one-dimensional shock waves and
one-dimensional Couette flow. The numerical scheme used here is based on Mieussens's
discrete velocity model (DVM). Computational results from the kinetic models are
compared to results obtained from the Direct Simulation Monte Carlo method (DSMC).
It is found that for hard sphere molecules the results obtained from the two new kinetic
models are very similar, and located in between the results from the ES-BGK and the
v(C)-BGK models, while for Maxwell molecules the two new kinetic models are
identical to the ES-BGK model. For one-dimensional shock waves, results from the new
kinetic model II fit best with results from DSMC; while for one-dimensional Couette
flow, the ES-BGK model is suggested.
Also in the second part of the work, a modified numerical scheme is developed from
Mieussens's original DVM. The basic idea is to use a linearized expression of the reference distribution function, instead of its exact expression, in the numerical scheme.
Results from the modified scheme are very similar to the results from the original scheme
for almost all done tests, while 20-40 percent of the computational time can be saved.
In the third part, several sets of macroscopic continuum equations are examined for
one-dimensional steady state Couette flow. For not too large Knudsen numbers
(Knc=O.l) in the transition regime, it is found that the original and slightly linearized
regularized 13 moment equations give better results than Grad's original 13 moment
equations, which, however, give better results than the Burnett equations, while the
Navier-Stokes-Fourier equations give the worst results, which is in agreement with the
expectation. For large Knudsen number situations (Kn>O.l), it turns out that all
macroscopic continuum equations tested fail in the accurate description of flows, while
the Grad's 13 moment equations can still give better results than the Burnett equations.
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AN EXPERIMENTAL METHOD FOR DETERMINING THE THERMAL ACCOMMODATION COEFFICIENT OF AN INERT GAS IN CONTACT WITH AN AMORPHOUS SURFACEConte, Richard Vincent, 1944- January 1977 (has links)
No description available.
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Hypersonic, low density flow past a wedge of finite lengthKlemm, Francis Joaquin 08 1900 (has links)
No description available.
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A conservative deterministic spectral method for rarefied gas flowsTharkabhushanam, Sri Harsha, 1979- 14 September 2012 (has links)
The mathematical analysis of the Boltzmann equation for a wide range of important models is well developed. It describes physical phenomena which are often of great engineering importance (in aerospace industry, semiconductor design, etc.). For that reason, analytical and computational methods of solving the Boltzmann equation are studied extensively. The idea of describing processes on a scale of the order of the relaxation scales of time and space has been realized. The nonlinear Boltzmann equation possesses the important essence of a physically realistic equation, so it is possible not only to consider the flows of simple media but to formulate new problems due to the ability of this equation to describe nonequilibrium states. In this dissertation, a new spectral Lagrangian based deterministic solver for the non-linear Boltzmann transport equation for variable hard potential (VHP) collision kernels with conservative or non-conservative binary interactions is proposed. The method is based on symmetries of the Fourier transform of the collision integral, where the complexity in the collision integral computation is reduced to a separate integral over the unit sphere S2. In addition, the conservation of moments is enforced by Lagrangian constraints. The resulting scheme, implemented in free space, is very versatile and adjusts in a very simple manner to several cases that involve energy dissipation due to local micro-reversibility (inelastic interactions) or to elastic model of slowing down processes. We prove the accuracy, consistency and conservation properties of the proposed conservative spectral method. Existing spectral methods have consistency proofs which are only for elastic collisions, and also such methods do not conserve all the necessary moments of the collision integral. In this dissertation, error estimates for the conservation routine are provided. Such conservation correction is implemented as an extended isoperimetric problem with the moment conservation properties as the constraints. We use and extend an existing bound estimate of Gamba, Panferov and Villani for the inelastic/elastic space homogeneous Boltzmann collision operator. The result is an original extension to the work of Gustaffson. Using these estimates along with projection error estimates and conservation correction estimates, we prove that the conservation correction is bounded by the spectral accuracy. Simulations are benchmarked with available exact self-similar solutions, exact moment equations and analytical estimates for the homogeneous Boltzmann equation for both elastic and inelastic VHP interactions. Benchmarking of the self-similar simulations involves the selection of a time rescaling of the numerical distribution function which is performed using the continuous spectrum of the equation for Maxwell molecules. The method also produces accurate results in the case of inelastic diffusive Boltzmann equations for hard-spheres (inelastic collisions under thermal bath), where overpopulated non-Gaussian exponential tails have been conjectured in computations by stochastic methods. Recognizing the importance of the Boltzmann equation in the analysis of shock structures and nonequilibrium states, such a study is done for 1D(x) × 3D(v). The classic Riemann problem is numerically analyzed for Knudsen numbers close to continuum. The shock tube problem of Sone and Aoki, where the wall temperature is suddenly changed, is also studied. We consider the problem of heat transfer between two parallel plates with diffusive boundary conditions for a range of Knudsen numbers from close to continuum to a highly rarefied state. Finally, the classical infinite shock tube problem that generates a non-moving shock wave is studied. The point worth noting is that the flow in the final case turns from a supersonic flow to a subsonic flow across the shock. / text
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A conservative deterministic spectral method for rarefied gas flowsTharkabhushanam, Sri Harsha, January 1900 (has links)
Thesis (Ph. D.)--University of Texas at Austin, 2008. / Vita. Includes bibliographical references and index.
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Using an expansion tube to generate rarefied hypervelocity gas flows /Chiu, Sam Hsieh-Hsiang. January 2004 (has links) (PDF)
Thesis (Ph.D.) - University of Queensland, 2005. / Includes bibliography.
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Simulation of gas dynamics, radiation and particulates in volcanic plumes on IoZhang, Ju, Goldstein, David B., Varghese, Philip L., January 2004 (has links) (PDF)
Thesis (Ph. D.)--University of Texas at Austin, 2004. / Supervisors: David B. Goldstein and Philip L. Varghese. Vita. Includes bibliographical references.
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Pressure Sensitive Paint Suitable to High Knudsen Number RegimeMori, Hideo, Niimi, Tomohide, Hirako, Madoka, Uenishi, Hiroyuki January 2006 (has links)
No description available.
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Modelling low-density flow in hypersonic impulse facilities /Wheatley, Vincent. January 2001 (has links) (PDF)
Thesis (M. Eng. Sc.)--University of Queensland, 2001. / Includes bibliographical references.
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A combined discrete velocity particle based numerical approach for continuum/rarefied flows /Roveda, Roberto, January 2000 (has links)
Thesis (Ph. D.)--University of Texas at Austin, 2000. / Vita. Includes bibliographical references (leaves 222-229). Available also in a digital version from Dissertation Abstracts.
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