@InCollection{HinckelSavoPati:2013:DeThLo,
author = "Hinckel, Jos{\'e} Nivaldo and Savonov, Roman I. and Patire Jr.,
Heitor",
title = "Determination of thermal load in film cooled bipropellant thrust
chambers by an inverse method",
booktitle = "Progress in Propulsion Physics",
publisher = "Torus Press",
year = "2013",
editor = "Wheeler, C. J.",
pages = "167--184",
address = "Moscou",
note = "This is an Open Access article distributed under the terms of the
Creative Commons Attribution License 2.0, which permits and
unrestricted use, distribution, and reproduction in any medium,
provided the original work is properly cited.",
keywords = "thermal load, bipropellant thrust chambers, film cooled.",
abstract = "A method to obtain the heat load on the internal wall of a rocket
thrust chamber using an inverse problem approach is described.
According to the classical approach, the heat load on the internal
wall of the chamber is assumed as the product of a heat transfer
coefficient and the temperature difference 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 coefficient profile. The
applicability of the method is verified by applying it to three
different problems; a model problem, an analytical solution, and a
set of experimental data.",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)}",
doi = "10.1051/eucass/201304167",
url = "http://dx.doi.org/10.1051/eucass/201304167",
isbn = "978-2-7598-0876-2",
label = "lattes: 1394917692174274 1 HinckelSavoPati:2013:DeThLo",
language = "en",
targetfile = "eucass4p167.pdf",
url = "http://dx.doi.org/10.1051/eucass/201304167",
volume = "4",
urlaccessdate = "01 maio 2024"
}