BibTex RIS Kaynak Göster

Influence of Swirl Number on Semi-Confined Flames

Yıl 2016, , 65 - 67, 12.07.2016
https://doi.org/10.18100/ijamec.69979

Öz

Stoichiometric methane air swirling flame has been modelled using RANS equations and a simplified mechanisms of reaction. The reaction zone is strongly affected by the swirl intensity. The higher the swirl number is, the narrower the reaction zone is. The thermodynamic state of reaction products matches well that of equilibrium state at constant pressure.

Kaynakça

  • Law C. K. Combustion Physics Cambridge. 2006
  • Chung T. J. "Computational Fluid Dynamics" Cambridge. 2006
  • Mira Martinez D., Cluff D.L., Jiang X., Numerical investigation of the burning characteristics of ventilation air methane in a combustion based mitigation system, Fuel Vol. 133 (2014) pp. 182–193 dx.doi.org/10.1016/j.fuel.2014.05.022
  • Chen Z., Ruan S., Swaminathan N. Simulation of turbulent lifted methane jet flames: Effects of air-dilution and transient flame propagation Combustion and Flame Vol. 162 (2015) pp. 703–716 dx.doi.org/10.1016/j.combustflame.2014.09.010
  • Ghasemi E., Soleimani S., Lin C.X. RANS simulation of methane-air burner using local extinction approach within eddy dissipation concept by OpenFOAM International Communications in Heat and Mass Transfer Vol 54 (2014) pp. 96–102 dx.doi.org/10.1016/j.icheatmasstransfer.2014.03.006
  • Parra T., Vuorinen V., Perez R., Szasz R. and Castro F.. Aerodynamic characterization of isothermal swirling flows in combustors. International Journal of Energy and Environmental Engineering (2014) 5:85.
  • Parra T., Perez R., Vuorinen V., Rodriguez M.A., Castro F. Flow features of confined swirling jets International Journal of Automotive Engineering and Technologies Vol. 4, Issue 1, 2015 pp. 12 – 15,
  • Roback R., Johnson B.V.. Mass and momentum turbulent transport experiments with confined swirling coaxial jets, NASA CR-168252, 1983
  • Kuo K. K. Principles of Combustion. Wiley Interscience. 1986
  • http://www.grc.nasa.gov/WWW/CEAWeb/ (visited 3.3.2015)

Original Research Paper

Yıl 2016, , 65 - 67, 12.07.2016
https://doi.org/10.18100/ijamec.69979

Öz

Kaynakça

  • Law C. K. Combustion Physics Cambridge. 2006
  • Chung T. J. "Computational Fluid Dynamics" Cambridge. 2006
  • Mira Martinez D., Cluff D.L., Jiang X., Numerical investigation of the burning characteristics of ventilation air methane in a combustion based mitigation system, Fuel Vol. 133 (2014) pp. 182–193 dx.doi.org/10.1016/j.fuel.2014.05.022
  • Chen Z., Ruan S., Swaminathan N. Simulation of turbulent lifted methane jet flames: Effects of air-dilution and transient flame propagation Combustion and Flame Vol. 162 (2015) pp. 703–716 dx.doi.org/10.1016/j.combustflame.2014.09.010
  • Ghasemi E., Soleimani S., Lin C.X. RANS simulation of methane-air burner using local extinction approach within eddy dissipation concept by OpenFOAM International Communications in Heat and Mass Transfer Vol 54 (2014) pp. 96–102 dx.doi.org/10.1016/j.icheatmasstransfer.2014.03.006
  • Parra T., Vuorinen V., Perez R., Szasz R. and Castro F.. Aerodynamic characterization of isothermal swirling flows in combustors. International Journal of Energy and Environmental Engineering (2014) 5:85.
  • Parra T., Perez R., Vuorinen V., Rodriguez M.A., Castro F. Flow features of confined swirling jets International Journal of Automotive Engineering and Technologies Vol. 4, Issue 1, 2015 pp. 12 – 15,
  • Roback R., Johnson B.V.. Mass and momentum turbulent transport experiments with confined swirling coaxial jets, NASA CR-168252, 1983
  • Kuo K. K. Principles of Combustion. Wiley Interscience. 1986
  • http://www.grc.nasa.gov/WWW/CEAWeb/ (visited 3.3.2015)
Toplam 10 adet kaynakça vardır.

Ayrıntılar

Bölüm Research Article
Yazarlar

M. Teresa Parra-santos

Ruben Perez Bu kişi benim

Victor Mendoza Bu kişi benim

Miguel A. Rodriguez Bu kişi benim

Francisco Castro Bu kişi benim

Yayımlanma Tarihi 12 Temmuz 2016
Yayımlandığı Sayı Yıl 2016

Kaynak Göster

APA Parra-santos, M. T., Perez, R., Mendoza, V., Rodriguez, M. A., vd. (2016). Influence of Swirl Number on Semi-Confined Flames. International Journal of Applied Mathematics Electronics and Computers, 4(3), 65-67. https://doi.org/10.18100/ijamec.69979
AMA Parra-santos MT, Perez R, Mendoza V, Rodriguez MA, Castro F. Influence of Swirl Number on Semi-Confined Flames. International Journal of Applied Mathematics Electronics and Computers. Ağustos 2016;4(3):65-67. doi:10.18100/ijamec.69979
Chicago Parra-santos, M. Teresa, Ruben Perez, Victor Mendoza, Miguel A. Rodriguez, ve Francisco Castro. “Influence of Swirl Number on Semi-Confined Flames”. International Journal of Applied Mathematics Electronics and Computers 4, sy. 3 (Ağustos 2016): 65-67. https://doi.org/10.18100/ijamec.69979.
EndNote Parra-santos MT, Perez R, Mendoza V, Rodriguez MA, Castro F (01 Ağustos 2016) Influence of Swirl Number on Semi-Confined Flames. International Journal of Applied Mathematics Electronics and Computers 4 3 65–67.
IEEE M. T. Parra-santos, R. Perez, V. Mendoza, M. A. Rodriguez, ve F. Castro, “Influence of Swirl Number on Semi-Confined Flames”, International Journal of Applied Mathematics Electronics and Computers, c. 4, sy. 3, ss. 65–67, 2016, doi: 10.18100/ijamec.69979.
ISNAD Parra-santos, M. Teresa vd. “Influence of Swirl Number on Semi-Confined Flames”. International Journal of Applied Mathematics Electronics and Computers 4/3 (Ağustos 2016), 65-67. https://doi.org/10.18100/ijamec.69979.
JAMA Parra-santos MT, Perez R, Mendoza V, Rodriguez MA, Castro F. Influence of Swirl Number on Semi-Confined Flames. International Journal of Applied Mathematics Electronics and Computers. 2016;4:65–67.
MLA Parra-santos, M. Teresa vd. “Influence of Swirl Number on Semi-Confined Flames”. International Journal of Applied Mathematics Electronics and Computers, c. 4, sy. 3, 2016, ss. 65-67, doi:10.18100/ijamec.69979.
Vancouver Parra-santos MT, Perez R, Mendoza V, Rodriguez MA, Castro F. Influence of Swirl Number on Semi-Confined Flames. International Journal of Applied Mathematics Electronics and Computers. 2016;4(3):65-7.