Showing 221 - 240 results of 2,808 for search '"São José dos Campos"', query time: 4.01s Refine Results
  1. 221
    by Gomes, Fábio Alexandre
    Published 2017
    ... pessoas com deficiência no município de São José dos Campos na região metropolitana do Vale do Paraíba. A...
    Get full text
    Others
  2. 222
  3. 223
  4. 224
  5. 225
  6. 226
    by Aline Campos Figueiredo
    Published 2012
    ... and the elementary school graduates career vision of the Municipal Public Schools of São José dos Campos, São Paulo...
    Get full text
    Others
  7. 227
  8. 228
    by Figueiredo, Mariana Leite
    Published 2007
    Subjects: ...Sindicatos - Metalúrgicos - São José dos Campos (SP)...
    Get full text
    Get full text
    Others
  9. 229
  10. 230
  11. 231
  12. 232
  13. 233
  14. 234
    by Luiz A. Magalhães, José F. de Carvalho
    Published 1973-09-01
    ... Belo Horizonte (MG) e de São José dos Campos (SP), Brasil. Concluiu-se que após a penetração das...
    Get full text
    Article
  15. 235
  16. 236
  17. 237
  18. 238
  19. 239
  20. 240
    by Izabel Cecilia Ferreira de Souza Vicentin, Carlos Henrique Marchi, Antonio Carlos Foltran, Diego Moro, Nicholas Dicati Pereira da Silva, Marcos Carvalho Campos, Luciano Kiyoshi Araki, J. Aerosp. Technol. Manag., São José dos Campos, v11, e3819, 2019 https://doi.org/10.5028/jatm.v11.1066 ORIGINAL PAPER 1.Universidade Federal do Paraná – Setor de Ciências Exatas – Engenharia Mecânica – Curitiba/PR – Brazil. 2.Universidade Positivo – Engenharia Mecânica – Curitiba/PR – Brazil. *Correspondence author: izabeldesouza@gmail.com Received: Feb. 6, 2018 | Accepted: Oct. 30, 2018 Section Editor: T John Tharakan ABSTRACT: Accurate determination of heat flux is an important task not only in the designing aspect, but also in the performance analysis of rocket engines. In this purpose, this work deals with the heat flux determination in a combustion chamber through the inverse method. In this approach, the transient heat flux is determined from the experimental temperature data measured at the outer sidewall of the rocket engine. In this work the physical phenomenon was modeled by the transient one-dimensional heat equation in cylindrical coordinates and the material properties of the chamber were considered constant. Furthermore, the model is solved using the inverse heat conduction problem with least squares modified by the addition of Tikhonov regularization term of zero-order. Moreover, the sensitivity coefficients were obtained by Duhamel’s theorem. Through the regularization parameter, it was able to generate acceptable results even when using data with considerable experimental errors. KEYWORDS: Combustion chambers, Heat flux, Heat conduction, Ill-posed problems. INTRODUCTION In a thrust chamber (nozzle and combustion chamber), the amount of energy transferred as heat to the chamber walls is between 0.5% and 5% of the total generated energy (Sutton 1992). Nevertheless, this amount could be enough to cause structural failure. Thus, to prevent the chamber and nozzle walls from failing, it is necessary to predict the heat flux accurately. Furthermore, accurate determination of heat flux is also important in the calculation of rocket engine performance and for the cooling system design. Convective and radiative heat transfer must be determined for characterization of total heat flux. The convective heat transfer coefficient typically depends on many fluid physical properties. The computation of the radiation heat transfer must be accounted by the surfaces emissivity and the absorption and scattering coefficients of the fluid mixture. However, information about these parameters is not always easily found. Considering the propellant applied in this work (potassium nitrate with sucrose, KNSu), the combustion products that affects radiation heat transfer are predominantly Theoretical and Experimental Heat Transfer in Solid Propellant Rocket Engine Izabel Cecilia Ferreira de Souza Vicentin1,*, Carlos Henrique Marchi1, Antonio Carlos Foltran1, Diego Moro1,2, Nicholas Dicati Pereira da Silva1, Marcos Carvalho Campos1, Luciano Kiyoshi Araki1, Alysson Nunes Diógenes
    Published 2019-08-01
    Get full text
    Article