@Article{Santos:2005:FlLeEf,
author = "Santos, Wilson Fernando dos",
affiliation = "{Instituto Nacional de Pesquisas Espaciais}",
title = "Flat-faced leading-edge effects in low-density hypersonic wedge
flow",
journal = "Journal of Spacecraft and Rockets",
year = "2005",
volume = "42",
number = "1",
pages = "22--29",
abstract = "A numerical study was performed to determine the upstream e®ects
of leading edge thickness on the rare¯ed hypersonic °ow over
truncated wedges at zero angle of attack. The simulations were
performed by using the Direct Simulation Monte Carlo (DSMC)
method. A method that has demonstrated to excellent comparisons
with °ight- and ground-test data, and properly accounts for
nonequilibrium aspects of the °ow that arise near the leading
edge, which are especially important at high Mach numbers. Some
signi¯cant di®erences between sharp and blunt leading edges were
noted on the °ow¯eld structure and on the aerodynamic surface
quantities. It was found that the upstream e®ects have di®erent
in°uence on the stagnation streamline properties ahead of the
leading edges depending on the leading edge Knudsen number.
Interesting features observed in the surface °uxes showed that
small leading edge thickness, compared to the freestream mean free
path, has important e®ects on high Mach number leading edge °ows.
Also, e®ects on the skin friction coe±cient, pressure coe±cient
and heat transfer coe±cient on the wedge are presented as a
function of thickness Knudsen number.",
issn = "0022-4650",
language = "en",
targetfile = "flatfaced.pdf",
urlaccessdate = "16 jun. 2024"
}