Direct Simulation Monte Carlo Method Applied to Aerothermodynamics



Título del documento: Direct Simulation Monte Carlo Method Applied to Aerothermodynamics
Revista: Journal of the Brazilian Society of Mechanical Sciences
Base de datos: PERIÓDICA
Número de sistema: 000312088
ISSN: 0100-7386
Autores: 1
Instituciones: 1Universidade Federal do Parana, Departamento de Fisica, Curitiba, Parana. Brasil
Año:
Volumen: 23
Número: 4
Paginación: 441-452
País: Brasil
Idioma: Inglés
Tipo de documento: Artículo
Enfoque: Experimental
Resumen en inglés An axisymmetric supersonic flow of rarefied gas past a finite cylinder was calculated applying the direct simulation Monte Carlo method. The drag force, the coefficients of pressure, of skin friction, and of heat transfer, the fields of density, of temperature, and of velocity were calculated as function of the Reynolds number for a fixed Mach number. The variation of the Reynolds number is related to the variation of the Knudsen number, which characterizes the gas rarefaction. The present results show that all quantities in the transition regime (Knudsen number is about the unity) are significantly different from those in the hydrodynamic regime, when the Knudsen number is small
Disciplinas: Física y astronomía,
Ingeniería
Palabras clave: Dinámica de fluidos,
Termodinámica y física estadística,
Ingeniería química,
Gases,
Flujo supersónico,
Gases enrarecidos,
Número de Knudsen,
Función de distribución,
Flujo externo
Keyword: Physics and astronomy,
Engineering,
Fluid dynamics,
Thermodynamics and statistical physics,
Chemical engineering,
Gas,
Supersonic flow,
Rarefied gas,
Knudsen number,
Distribution number,
External flow
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