Compressible Flows
Mostrando 13-24 de 35 artigos, teses e dissertações.
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13. Development and testing of high-resolution upwind schemes and their applications in incompressible free surface flows / Desenvolvimento e teste de esquemas "upwind" de alta resolução e suas aplicações em escoamentos incompressíveis com superfícies livres
Neste trabalho são apresentados os resultados do desenvolvimento e teste de esquemas upwind de alta resolução para o controle da difusão numérica em leis de conservação gerais e problemas em dinâmica dos fluidos. Em particular, são derivados dois novos esquemas: o ALUS (Adaptive Linear Upwind Scheme) e o TOPUS (Third-Order Polynomial Upwind Scheme).
Publicado em: 2009
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14. Aeroacústica e instabilidades de uma camada de mistura compressível / Flow instability and aeroacoustics of a compressible mixing layer
Tanto os motores turbo-jato quanto os turbo-fan, são os maiores responsáveis pela geração de ruído durante a decolagem, segmento de subida e de aceleração de uma aeronave. Devido a isto, o problema de ruído em jatos vem sendo intensamente investigado ao longo dos últimos anos. Já na fase do pouso, o slat é uma das fontes de ruído mais importantes
Publicado em: 2009
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15. An adaptive mesh strategy for high compressible flows based on nodal re-allocation
An adaptive mesh strategy based on nodal re-allocation is presented in this work. This technique is applied to problems involving compressible flows with strong shocks waves, improving the accuracy and efficiency of the numerical solution. The initial mesh is continuously adapted during the solution process keeping, as much as possible, mesh smoothness and l
Journal of the Brazilian Society of Mechanical Sciences and Engineering. Publicado em: 2008-09
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16. NUMERICAL STUDY OF THE INTERACTION BETWEEN A SUPERSONIC JET AND PLANAR SURFACE / ESTUDO NUMÉRICO DA INTERAÇÃO ENTRE UM JATO SUPERSÔNICO E UMA SUPERFÍCIE PLANA
I in this work a study of the interaction between a supersonic jet and a planar surface is presented, with the aim to analyze the behavior of the velocity, pressure and temperature flowfield. This study finds its motivation in the process of thermal spallation of hard rocks, which may result from the interaction between a high pressure and high temperature j
Publicado em: 2008
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17. AnÃlise de escoamentos compressÃveis nÃo-viscosos em trÃs dimensÃes utilizando o mÃtodo dos elementos finitos por aresta
This work has as its main goal the development of a computational tool for numerical simulation of compressible fluid flow problems for three dimensions, using as starting point the computational tool developed by LYRA (1994) that dealt with fluid flow problems in two dimensional domain. For the development of this tool, a space discretization was adopted us
Publicado em: 2008
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18. A numerical model for thin airfoils in unsteady compressible arbitrary motion
A numerical method based on the vortex methodology is presented in order to obtain unsteady solution of the aerodynamic coefficients of a thin airfoil in either compressible subsonic or supersonic flows. The numerical model is created through the profile discretization in uniform segments and the compressible flow vortex singularity is used. The results of t
Journal of the Brazilian Society of Mechanical Sciences and Engineering. Publicado em: 2007-09
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19. Advanced turbulence modelling for complex aerospace applications.
The objective of the present research work consists in studying complex aerodynamic flows about typical aerospace configuration, in which turbulence effects play a fundamental role. Such study is performed with an available computational tool that is being developed at CTA/IAE. This is a finite-volume code for unstructured 3-D meshes that solves the compress
Publicado em: 2007
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20. Numerical analysis of the turbulent coaxial jets / Análise numérica de jatos coaxiais turbulentos
The understanding of the jets behavior is of extreme importance in several practical applications in combustion and propulsion. Therefore, it becomes more and more important the detailed analysis of the parameters that affect the characteristics of this type of flow. This work presents a numerical study of the incompressible turbulent coaxial jets characteri
Publicado em: 2007
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21. Compressible shear layer direct numerical simulation / Simulação numérica direta de camada cisalhante compressível com fonte de calor
No presente trabalho são feitas uma simulação numérica direta (SND) de camada de mistura em regime compressível com fonte de calor em seu interior, numa análise temporal bidimensional para um escoamento em regime subsonico. A fonte de calor apresenta-se como um modelo simplificado de um escoamento reativo. A simulação parte de um escoamento laminar a
IBICT - Instituto Brasileiro de Informação em Ciência e Tecnologia. Publicado em: 12/12/2006
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22. A comparison of hyperbolic solvers for ideal and real gas flows
Classical and recent numerical schemes for solving hyperbolic conservation laws were analyzed for computational efficiency and application to nonideal gas flows. The Roe-Pike approximate Riemann solver with entropy correction, the Harten second-order scheme and the extension of the Roe-Pike method to second-order by the MUSCL strategy were compared for one-d
Brazilian Journal of Chemical Engineering. Publicado em: 2006-09
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23. Numerical simulations of compressible flows over airfoils.
A computer code was developed from scratch to simulate the flow over the NACA 0012 airfoil at different Reynolds and Mach numbers. The domain was discretized in a structured-grid context. The equations were numerically solved by a finite-volume technique, using three different time-marching schemes. The Euler flow was initially modeled as well as a Reynolds-
Publicado em: 2006
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24. Simulação numérica direta de camada cisalhante compressível com fonte de calor / Compressible shear layer direct numerical simulation
No presente trabalho são feitas uma simulação numérica direta (SND) de camada de mistura em regime compressível com fonte de calor em seu interior, numa análise temporal bidimensional para um escoamento em regime subsonico. A fonte de calor apresenta-se como um modelo simplificado de um escoamento reativo. A simulação parte de um escoamento laminar a
Publicado em: 2006