@InProceedings{PalhariniSant:2010:SuTeEf,
author = "Palharini, Rodrigo C. and Santos, Wilson Fernando Nogueira",
affiliation = "{} and {Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Surface temperature effects on the aerodynamic surface quantities
of hypersonic cavity flow",
booktitle = "Anais...",
year = "2010",
organization = "Simp{\'o}sio de Mec{\^a}nica Computacional.",
publisher = "Universidade Federal de S{\~a}o Jo{\~a}o del-Rei",
address = "S{\~a}o Jo{\~a}o del-Rei, MG",
keywords = "hypersonic flow, rarefied flow, DSMC, cavity, aerodynamic
heating.",
abstract = "Abstract. Numerical simulations of two-dimensional steady
hypersonic flow in a rectangular cavity at different
length-to-depth (L=H) ratio and wall temperature are performed by
using a Direct Simulation Monte Carlo (DSMC) method. The L=H ratio
varies from 1 to 4 and wall temperature ranges from 2 to 6 times
the freestream temperature. The work focuses on the effect in the
aerodynamic surface quantities, such as heat transfer, pressure
and skin friction coefficients due to variations in the cavity L=H
ratio as well as in the wall temperature. It was found that the
aerodynamic surface quantities presented a large dependence on the
L=H ratio, and a small dependence on the wall temperature for the
range investigated. The analysis showed that pressure and heating
loads presented the maximum values along the downstream face, more
precisely, at the shoulder of the cavities. Moreover, pressure and
heating loads are several times larger than those for a smooth
surface.",
conference-location = "S{\~a}o Jo{\~a}o del-Rei, MG",
conference-year = "26-28 Maio",
language = "en",
organisation = "Universidade Federal de S{\~a}o Jo{\~a}o del-Rei",
targetfile = "surface.pdf",
urlaccessdate = "09 maio 2024"
}