@InProceedings{SantosLewi:2004:EfCoRa,
author = "Santos, Wilson Fernando Nogueira dos and Lewis, M. J.",
affiliation = "{Instituto Nacional de Pesquisas Espaciais} and {University of
Maryland}",
title = "The effect of compressibility on rarefied hypersonic flow over
power law leading edges.",
booktitle = "Proceedings...",
year = "2004",
organization = "AIAA Aerospace Sciences Meeting and Exhibit, 42.",
publisher = "AIAA",
address = "Washington, DC",
note = "{AIAA Paper 2004-1181}",
keywords = "hypersonic flow, rarefied flow, DSMC, power law shapes, blunt
leading edges.",
abstract = "Hypersonic flow past power law shaped leading edges at zero
incidence is investigated for a range of freestream Mach number
from 5 to 12. The simulations were performed by using a Direct
Simulation Monte Carlo Method. A method that has demonstrated to
yield excellent comparison with experimental data, and that
properly accounts for thermal nonequilibrium effects that arise
near the leading edge and that are especially important at high
Mach number. The work is motivated by interest in assessing the
overall performance of power-law shaped leading edges in order to
consider them as possible candidates for blunting geometries of
hypersonic leading edges. The results presented highlight the
sensitivity of the heat transfer coe±cient, the total drag
coefficient, and the shock wave standoff distance to changes on
the freestream Mach number.",
conference-location = "Reno, NV, USA",
conference-year = "5-8 Jan. 2004",
copyholder = "SID/SCD",
language = "en",
targetfile = "effectAIAA.pdf",
urlaccessdate = "08 maio 2024"
}