@InProceedings{CoutoPimeBast:2002:LoPrIn,
               author = "Couto, Haroldo da Silva and Pimenta, A. P. and Bastos Neto, 
                         Dem{\'e}trio",
          affiliation = "{} and ITA",
                title = "Low pressure injection system for small liquid propellant rocket 
                         engines",
                 year = "2002",
                pages = "374--378",
         organization = "Asia Pacific International Symposium on Combustion and Energy 
                         Utilization, 6.",
             keywords = "COMBUSTAO, low pressure.",
             abstract = "In this paper a numerical study is reported on sharp/blunt leading 
                         edges in a rarefied hypersonic flow. The purpose of this paper is 
                         to investigate the sensitivity of both the flowfield structure and 
                         surface quantities to leading edge thickness variations. DSMC 
                         results indicate that even though for a slightly blunt leading 
                         edge, thickness of one hundredth of the mean free path, the flow 
                         structure was affected far from the nose of the leading edge. 
                         Also, substantial increase in the surface quantities is observed 
                         as the leading edge thickness increases.",
  conference-location = "Kuala Lumpur",
      conference-year = "20-22 May 2002",
           copyholder = "SID/SCD",
                label = "10506",
           targetfile = "couto.pdf",
        urlaccessdate = "04 maio 2024"
}