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Aerothermodynamic comparison of two- and three-dimensional rarefied hypersonic cavity flow

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

Resumen

Hypersonic flow over two-and three-dimensional rectangular cavities at different lengthto-depth (L/D) ratio are performed using the direct simulation Monte Carlo (DSMC) method. The work focuses on the impact on the aerodynamic surface quantities due to variations in the length-to-depth ratio and cavity three-dimensional effects. The analysis showed that the aerodynamic quantities acting on the cavity surface depends heavily on the three-dimensional flow characteristics as well as the cavity L/D ratio. Furthermore, two-dimensional cavity study over-predict heat and pressure loads, with these being several times larger than those observed for a three-dimensional cavity.

Idioma originalInglés
Título de la publicación alojada43rd AIAA Thermophysics Conference 2012
EditorialAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (versión impresa)9781624101861
DOI
EstadoPublicada - 2012
Publicado de forma externa
Evento43rd AIAA Thermophysics Conference 2012 - New Orleans, LA, Estados Unidos
Duración: 25 jun 201228 jun 2012

Serie de la publicación

Nombre43rd AIAA Thermophysics Conference 2012

Conferencia

Conferencia43rd AIAA Thermophysics Conference 2012
País/TerritorioEstados Unidos
CiudadNew Orleans, LA
Período25/06/1228/06/12

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