@InProceedings{Santos:2004:PaIISh,
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 III - shock wave structure",
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: Computations using the Direct Simulation Monte Carlo
(DSMC) method are presented for hypersonic flow over flat-nose
leading edges. The primary aim of this paper is to examine the
effect of the body surface temperature on the shock wave
structure. The sensitivity of shock wave shape, shock standoff
distance, and shock thickness to wall temperature variations is
calculated by using a model that classifies the molecules in three
distinct classes, i.e., undisturbed freestream, reflected from the
boundary and scattered, i.e., molecules that had been indirectly
affected by the presence of the leading edge. The analysis shows
significant differences on the shock wave structure due to
variations on the body surface temperature. It was found that the
flat-nose leading edges provided smaller shock wave standoff
distance and shock wave thickness, compared to the corresponding
circular cylinder that generated the flat-nose bodies.",
conference-location = "Rio de Janeiro, RJ",
conference-year = "29 Nov. - 3 Dez. 2004",
language = "en",
targetfile = "surface 3.pdf",
urlaccessdate = "16 jun. 2024"
}