@InProceedings{Santos:2005:GaImAe,
author = "Santos, Wilson Fernando Nogueira",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Gas-surface impact on aerodynamic surface quantities of
low-density hypersonic flow over flat-nose bodies",
booktitle = "Proceedings...",
year = "2005",
organization = "International Congress of Mechanical Engineering, 18. (COBEM).",
publisher = "ABCM",
address = "Rio de Janeiro, RJ",
keywords = "hypersonic flow, rarefied flow, DSMC, blunt leading edge,
gas-surface accommodation.",
abstract = "ABSTRACT: The present work performs a computational study on
rarefied hypersonic flow past flat-nose leading edges at zero
incidence. Effects of incomplete surface accommodation on the
aerothermodynamic surface quantities have been investigated by
employing the Direct Simulation Monte Carlo (DSMC) method in
combination with the Cercignani-Lampis-Lord gas surface
interaction model, which incorporates separate accommodation
coefficients for normal and tangential velocity components. The
work also focuses the attention of designers of hypersonic
configurations on the fundamental parameter of bluntness, which
can have an important impact on even initial design. The results
presented highlight the sensitivity of the heat transfer and drag
coefficients to changes on the gas-surface accommodation
coefficients. These are compared to the results for classical
diffuse reflection model. It was found that stagnation point
heating decreased by a reduction on the normal accommodation
coefficient and the total drag decreased by a reduction on the
tangential accommodation coefficient.",
conference-location = "Ouro Preto, MG",
conference-year = "06-11 Nov. 2005",
copyholder = "SID/SCD",
language = "en",
targetfile = "gas-surfaceimpa1.pdf",
urlaccessdate = "10 maio 2024"
}