@InProceedings{Santos:2008:SoExUn,
               author = "Santos, Wilson Fernando Nogueira",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)}",
                title = "Some extensions to the underwedge-surface angle effects on the 
                         flowfield structure of a sharp leading edge in hypersonic flow",
            booktitle = "Proceedings...",
                 year = "2008",
         organization = "Encontro de Modelagem Computacional, 11.",
            publisher = "UERJ",
              address = "Rio de Janeiro",
             keywords = "hypersonic flow, rarefied flow, DSMC, sharp leading edge, 
                         flat-plate.",
             abstract = "A computational investigation of the rarefied hypersonic flow over 
                         a flat plate with a sharp leading edge is presented. A Direct 
                         Simulation Monte Carlo (DSMC) method is applied to obtain a 
                         non-equilibrium state for the rarefied gas flow over the flat 
                         plate. Results for a flat plate with five different 
                         underwedge-surface angles and three wall temperatures are compared 
                         in order to assess the relative importance of the 
                         underwedge-surface angle and the wall temperature on the 
                         aerodynamic surface quantities. From these numerical simulations, 
                         interesting features were observed in the surface fluxes. It was 
                         found that small underwedge-surface angle has important effects on 
                         high Mach number leading edge flows.",
  conference-location = "Volta Redonda, RJ",
      conference-year = "17-19 nov.",
           targetfile = "some.pdf",
        urlaccessdate = "16 jun. 2024"
}