@InProceedings{HinckelSavoPati:2011:DeThLo,
               author = "Hinckel, Jose Nivaldo and Savonov, Roman and Patire Jr., Heitor",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "Determination of thermal load in film cooled bipropellant thrust 
                         chambers by an inverse method",
                 year = "2011",
         organization = "European Conference For Aerospace Sciences, 4.",
             keywords = "rocket thrust chamber, inverse problem approach, heat transfer.",
             abstract = "This paper describes a method to obtain the heat load on the 
                         internal wall of a rocket thrust chamber using an inverse problem 
                         approach. According to the classical approach, the heat load on 
                         the internal wall of the chamber is assumed as the product of a 
                         heat transfer coecient and the temperature dierence of adiabatic 
                         wall temperature and local wall surface temperature. The time 
                         dependent temperature distribution of the external wall of the 
                         thruster chamber is used to obtain empirical curve fittings to the 
                         temperature profile of the near wall flow field (adiabatic wall 
                         temperature) and the heat transfer coecient profile. The 
                         applicability of the method is verified by applying it to three 
                         dierent problems; a model problem, an analytical solution, and a 
                         set of experimental data.",
             language = "en",
           targetfile = "Hinckel_et_al_2011.pdf",
        urlaccessdate = "12 maio 2024"
}