@InProceedings{LeiteSant:2014:CoEfCo,
author = "Leite, Paulo Henrique Mineiro and Santos, Wilson Fernando Nogueira
dos",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Compressibility Effects on Combined Gap/Step Geometries at
Rarefied Hypersonic Flow",
booktitle = "Proceedings...",
year = "2014",
organization = "World Congress on Computational Mechanics (WCCM XI), 11. /
European Conference on Computational Mechanics (ECCM V), 5 /
European Conference on Computational Fluid Dynamics (ECFD VI), 6",
note = "{Setores de Atividade: Pesquisa e desenvolvimento
cient{\'{\i}}fico.}",
keywords = "DSMC, Hypersonic Flow, Rarefied Flow, Forward-Facing Step, Gap,
Compressibility Effects.",
abstract = "It is generally recognized that the physical phenomena related to
the problem of separation are very important in the design of
hypersonic configurations. When separation occurs in high Mach
number flows, changes in pressure distribution and heat transfer
rate may have catastrophic effects in the vehicle. The presence of
hot spots at separation and reattachment points changes the
characteristics of the flow over the vehicle and can cause failure
in the thermal protection system, as was evidenced by the tragic
loss of Space Shuttle Columbia in 2003. In general, separation
occurs due to the interaction of external flows with various
desired or undesired design features present on the vehicle
surface, such as protuberances, notches, cavities, gaps, or
steps.",
conference-location = "Barcelona, Spain",
conference-year = "July 20-25, 2014",
label = "lattes: 4859685163568596 2 LeiteSant:2014:CoEfCo",
language = "en",
targetfile = "a3132.pdf",
urlaccessdate = "27 abr. 2024"
}