12 results on '"Direct Simulation"'
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2. Construction and optimization of numerically-statistical projection algorithms for solving integral equations.
- Author
-
Korda, Anna S., Mikhailov, Gennady A., and Rogasinsky, Sergey V.
- Subjects
- *
INTEGRAL equations , *LAGUERRE polynomials , *MONTE Carlo method , *ALGORITHMS , *PROBLEM solving - Abstract
The problem of minimizing the root-mean-square error of the numerical-statistical projection estimation of the solution to an integral equation is solved. It is shown that the optimal estimator in this sense can be obtained by equalizing deterministic and stochastic components of the error in the case when the norm of the remainder of the utilized decomposition decreases inversely proportional to its length. As a test, the Milne problem of radiation transfer in a semi-infinite layer of matter is solved using Laguerre polynomials. To solve such a problem in the case of a finite layer, a special regularized projection algorithm is used. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
3. Comparative Analysis of Numerical-Statistical Projection Algorithms for Solving Transfer Theory Problems.
- Author
-
Mikhailov, G. A., Korda, A. S., and Rogasinsky, S. V.
- Subjects
- *
GRANULAR flow , *COMPARATIVE studies , *MONTE Carlo method , *LAGUERRE polynomials - Abstract
A comparative analysis of various projection Monte Carlo algorithms as applied to estimating the particle flow through a layer of medium with scattering of the Henyey–Greenstein type is carried out. The possibility of minimizing the mean-square error by equalizing the corresponding stochastic and deterministic terms is investigated. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
4. Inverse Problem of Finding Surface Roughness Parameters in Rarefied Gas Flow.
- Author
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Aksenova, Olga A. and Khalidov, Iskander A.
- Subjects
- *
INVERSE problems , *SURFACE roughness , *GAS flow - Abstract
The new algorithm is proposed to determine the real values of the roughness parameter σ1 from aerodynamic measurements solving the inverse problem. Roughness parameters are measured usually in the experiment from the profile diagram. However, the main parameter defining surface roughness according to usual standard procedures is not σ1, but the square mean deviation σ of the height of the surface. The roughness parameter in rarefied gas σ1 is not measured in the experiments. In addition, even if the parameter σ1 is measured, the main input into the influence of surface roughness on aerodynamic values takes the roughness of smaller scale, usually negligible on the profile diagram. Therefore σ1 must be determined from the solution of the inverse problem. The solution of the inverse problem is based on the simulation of surface roughness on micro-level by Gaussian or poly-Gaussian random field and on the representation of the scattering function on rough surface. The main advantage of the model is based on relative simple relations between the parameters of the model and the basic statistical characteristics of random field. Considered statistical approach permits to apply not only diffuse-specular model of the local scattering function of reflected gas atoms, but also Cercignani–Lampis scattering kernel or phenomenological models of scattering function. From the results we can see that the value of σ1 obtained from the solution of inverse problem is substantially higher than the value of σ1 from the profile diagram measurements. [ABSTRACT FROM AUTHOR]
- Published
- 2019
- Full Text
- View/download PDF
5. Analytic Model of the Effect of Poly-Gaussian Roughness on Rarefied Gas Flow near the Surface.
- Author
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Aksenova, Olga A. and Khalidov, Iskander A.
- Subjects
- *
RAREFIED gas dynamics flow , *SURFACE roughness measurement , *SURFACES (Physics) , *KNUDSEN flow , *GAS mixtures - Abstract
The dependence of the macro-parameters of the flow on surface roughness of the walls and on geometrical shape of the surface is investigated asymptotically and numerically in a rarefied gas molecular flow at high Knudsen numbers. Surface roughness is approximated in statistical simulation by the model of poly-Gaussian (with probability density as the mixture of Gaussian densities [1]) random process. Substantial difference is detected for considered models of the roughness (Gaussian, poly-Gaussian and simple models applied by other researchers), as well in asymptotical expressions [3], as in numerical results. For instance, the influence of surface roughness on momentum and energy exchange coefficients increases noticeably for poly-Gaussian model compared to Gaussian one (although the main properties of poly-Gaussian random processes and fields are similar to corresponding properties of Gaussian processes and fields). Main advantage of the model is based on relative simple relations between the parameters of the model and the basic statistical characteristics of random field. Considered statistical approach permits to apply not only diffusespecular model of the local scattering function V0 of reflected gas atoms, but also Cercignani-Lampis scattering kernel or phenomenological models of scattering function. Thus, the comparison between poly-Gaussian and Gaussian models shows more significant effect of roughness in aerodynamic values for poly-Gaussian model. [ABSTRACT FROM AUTHOR]
- Published
- 2016
- Full Text
- View/download PDF
6. Poly-Gaussian Model of Randomly Rough Surface in Rarefied Gas Flow.
- Author
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Aksenova, Olga A. and Khalidov, Iskander A.
- Subjects
- *
RAREFIED gas dynamics flow , *GAUSSIAN processes , *ROUGH surfaces , *PROBABILITY density function , *MONTE Carlo method , *SCATTERING (Physics) - Abstract
Surface roughness is simulated by the model of non-Gaussian random process. Our results for the scattering of rarefied gas atoms from a rough surface using modified approach to the DSMC calculation of rarefied gas flow near a rough surface are developed and generalized applying the poly-Gaussian model representing probability density as the mixture of Gaussian densities. The transformation of the scattering function due to the roughness is characterized by the roughness operator. Simulating rough surface of the walls by the poly-Gaussian random field expressed as integrated Wiener process, we derive a representation of the roughness operator that can be applied in numerical DSMC methods as well as in analytical investigations. [ABSTRACT FROM AUTHOR]
- Published
- 2014
- Full Text
- View/download PDF
7. On-line inference for multiple changepoint problems.
- Author
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Fearnhead, Paul and Zhen Liu
- Subjects
SIMULATION methods & models ,PARTICLES ,MONTE Carlo method ,MATHEMATICAL models ,STRATIFIED sets ,ALGORITHMS - Abstract
We propose an on-line algorithm for exact filtering of multiple changepoint problems. This algorithm enables simulation from the true joint posterior distribution of the number and position of the changepoints for a class of changepoint models. The computational cost of this exact algorithm is quadratic in the number of observations. We further show how resampling ideas from particle filters can be used to reduce the computational cost to linear in the number of observations, at the expense of introducing small errors, and we propose two new, optimum resampling algorithms for this problem. One, a version of rejection control, allows the particle filter to choose the number of particles that are required at each time step automatically. The new resampling algorithms substantially outperform standard resampling algorithms on examples that we consider; and we demonstrate how the resulting particle filter is practicable for segmentation of human G+C content. [ABSTRACT FROM AUTHOR]
- Published
- 2007
- Full Text
- View/download PDF
8. On the Formation and Accumulation of Solid Carbon Particles in High-Enthalpy Flows Mimicking Re-Entry in the Titan Atmosphere
- Author
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Mario Commodo, Marcello Lappa, Gennaro Zuppardi, Christophe Allouis, Antonio Esposito, Patrizia Minutolo, Barbara Apicella, and Carmela Russo
- Subjects
hypersonic flow ,Materials science ,Enthalpy ,Analytical chemistry ,02 engineering and technology ,lcsh:Thermodynamics ,solid particles ,01 natural sciences ,Methane ,010305 fluids & plasmas ,symbols.namesake ,chemistry.chemical_compound ,020401 chemical engineering ,lcsh:QC310.15-319 ,0103 physical sciences ,0204 chemical engineering ,Atmosphere of Titan ,Spectroscopy ,Direct Simulation ,lcsh:QC120-168.85 ,Fluid Flow and Transfer Processes ,Mechanical Engineering ,methane ,chemical reactions ,Tholin ,arc-heated facility ,Condensed Matter Physics ,Monte Carlo method ,TA ,chemistry ,symbols ,lcsh:Descriptive and experimental mechanics ,Direct simulation Monte Carlo ,Titan (rocket family) ,Raman spectroscopy - Abstract
The problem relating to the formation of solid particles enabled by hypersonic re-entry in methane-containing atmospheres (such as that of Titan) has been tackled in the framework of a combined experimental&ndash, numerical approach implemented via a three-level analysis hierarchy. First experimental tests have been conducted using a wind tunnel driven by an industrial arc-heated facility operating with nitrogen as working gas (the SPES, i.e., the Small Planetary Entry Simulator). The formation of solid phases as a result of the complex chemical reactions established in such conditions has been detected and quantitatively measured with high accuracy. In a second stage of the study, insights into the related formation process have been obtained by using multispecies models relying on the NASA CEA code and the Direct Simulation Monte Carlo (DSMC) method. Through this approach the range of flow enthalpies in which carbonaceous deposits can be formed has been identified, obtaining good agreement with the experimental findings. Finally, the deposited substance has been analyzed by means of a set of complementary diagnostic techniques, i.e., SEM, spectroscopy (Raman, FTIR, UV&ndash, visible absorption and fluorescence), GC&ndash, MS and TGA. It has been found that carbon produced by the interaction of the simulated Titan atmosphere with a solid probe at very high temperatures can be separated into two chemically different fractions, which also include &ldquo, tholins&rdquo
- Published
- 2020
- Full Text
- View/download PDF
9. Determination of plume impingement disturbance characteristics for the ROCSAT-1 satellite.
- Author
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Yang, A-S and Kuo, T-C
- Subjects
PLUMES (Fluid dynamics) ,ARTIFICIAL satellites ,AEROSPACE engineering - Abstract
The impingement disturbance characteristics of the hydrazine thruster plumes have been examined comprehensively for the ROCSAT-1 satellite. In this study, the velocity and temperature distributions at the nozzle exit are obtained from the nozzle flowfield analysis. The axial velocity, transverse velocity and temperature profiles are further correlated with the curve-fitting procedure for resolving inflow properties of molecules ejected into a vacuum. The free-molecular direct simulation M onte Carlo technique is used to describe the particle nature of the distant plume flow behaviour near the impingement surface. The inflow molecular motions as well as the collision interactions between the molecules and the solid surface are treated on a probabilistic basis. On the other hand, the intercollisions among molecules are considered to be relatively unimportant in the far-field plume region. A reasonable number of simulated molecules is also employed to reproduce the fluid behaviour in the macroscopic level. The predicted disturbance torques and thrust loss are found to be much less than the design control torques and the nominal thrust force for ROCSAT-1 satellite, indicating that the plume impingement effect will not cause any performance deterioration of the propulsive function. [ABSTRACT FROM AUTHOR]
- Published
- 2002
- Full Text
- View/download PDF
10. Hypersonic rarefied flows DSMC analysis by a simplified chemical model.
- Author
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Cercignani, Carlo, Frezzotti, Aldo, and Sibilla, Stefano
- Abstract
Copyright of Meccanica is the property of Springer Nature and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
- Published
- 1995
- Full Text
- View/download PDF
11. Monte Carlo simulation of the propagation of a disturbance in the channel flow of a rarefied gas
- Author
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Stefan Stefanov and Carlo Cercignani
- Subjects
Disturbance (geology) ,Monte Carlo method ,Mechanics ,Open-channel flow ,Direct simulation ,Physics::Fluid Dynamics ,Computational Mathematics ,Computational Theory and Mathematics ,Modeling and Simulation ,Modelling and Simulation ,Kinetic theory of gases ,Dynamic Monte Carlo method ,Statistical physics ,Direct simulation Monte Carlo ,Kinetic theory ,Channel flow ,Mathematics ,Communication channel - Abstract
We report and discuss the results of a Direct Monte Carlo Simulation of the propagation of a disturbance in a rarefied gas flowing in a channel.
- Published
- 1998
- Full Text
- View/download PDF
12. Direct Monte Carlo Calculation on Heat Transfer through a Rarefied Gas
- Author
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Usami, Masaru, Fujimoto, Tetsuo, and Kato, Seizo
- Subjects
direct simulation ,Monte Carlo method ,spine-fin ,heat transfer ,rarefied gas - Abstract
The direct simulation Monte Carlo method is used for analysis of a heat transfar from a spine-fin through a rarefied gas. The heat flux which flows from a base of the spine through its cross-section is transferred from a surface of the spine by molecular motion and radiation. Two types of time scale are required ; one is for the molecular motion and the other is for appreciable change of the spine temperature. Since the latter time scale is several orders larger than the former, a weighting factor of the time scale is used to compensate for the large time disparities. The results of the calculation are compared with those of experiment.
- Published
- 1989
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