@InProceedings{Santos:2004:AeSuQu,
author = "Santos, Wilson Fernando Nogueira dos",
affiliation = "{Instituto Nacional de Pesquisas Espaciais}",
title = "Surface temperature effects in low-density flow over flat-nose
bodies at hypersonic speeds, Part 2 - aerodynamic surface
quantities",
booktitle = "Proceedings...",
year = "2004",
organization = "Brazilian Congress of Thermal Sciences and Engineering, 10.
(ENCIT).",
publisher = "ABCM",
address = "Rio de Janeiro, RJ",
keywords = "hypersonic flow, rarefied flow, blunt leading edges, DSMC.",
abstract = "ABSTRACT: The successful design of high-lift, low-drag hypersonic
configurations depends on the ability to incorporate sharp/blunt
leading edges that combine good aerodynamic properties with
acceptable heating rates. In this study, the hypersonic
two-dimensional flow around a family of flat-nose leading edges at
zero incidence is investigated by using the Direct Simulation
Monte Carlo (DSMC) method. Effects of variation on the body
surface temperature and on the leading edge thickness are
investigated in terms of the aerodynamic surface quantities. The
aerothermodynamic performance of the flat-nose leading edges is
assessed by using the pressure, skin friction, heat transfer and
total drag coefficients. The calculation results depict a weak
effect of the leading edge thickness and of the wall temperature
on total drag, while predict a strong dependence of stagnation
point heating on the leading edge thickness over the range
examined. The data generated in the present study is part of an
investigation in order to determine the benefits and disadvantages
of using these new blunt shapes over circular cylinder shapes.",
conference-location = "Rio de Janeiro, RJ",
conference-year = "29 Nov. - 3 Dez. 2004",
copyholder = "SID/SCD",
language = "en",
targetfile = "surface 2.pdf",
urlaccessdate = "16 jun. 2024"
}