مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

696
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

0
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

NUMERICAL AND ANALYTICAL INVESTIGATION OF SHOCK TRAIN IN A CONVERGENT DIVERGENT NOZZLE

Pages

  101-112

Abstract

 In the present work, the SHOCK TRAIN structure in a convergent-divergent nozzle investigated using large eddy simulation (LES) methodology based on different SUBGRID MODELS, including Smagorinsky-Lilly (SL), Wall-Adapting Local Eddy-Viscosity (WALE) and Algebraic Wall-Modeled LES (WMLES) as well as various analytical equations. For gaining a distinct illustration of shock-wave structures, shadowgraph contours are applied to analyze structures of fine flow. The simulated results are obtained at the same geometrical and boundary conditions used in the available experimental data to provide a rational validation. The results of different SUBGRID MODELS are shown that the WMLES produces more accurate results than SL and WALE models. Thereupon, an investigation of the influence of convergency length and discontinuity of nozzle wall temperature on physics of flow for controlling the shock behavior is carried out. The results show that the minimum wall pressure as well as the maximum flow Mach number increase as the convergency length rises. In addition, by growth in discontinuous wall temperature, the minimum wall pressure and the maximum flow Mach number reduce.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    KAMALI, R., MOUSAVI, S.M., HOUSHYARI, P., & KHANEH ZAR, A.. (2017). NUMERICAL AND ANALYTICAL INVESTIGATION OF SHOCK TRAIN IN A CONVERGENT DIVERGENT NOZZLE. JOURNAL OF SOLID AND FLUID MECHANICS, 7(1 ), 101-112. SID. https://sid.ir/paper/212710/en

    Vancouver: Copy

    KAMALI R., MOUSAVI S.M., HOUSHYARI P., KHANEH ZAR A.. NUMERICAL AND ANALYTICAL INVESTIGATION OF SHOCK TRAIN IN A CONVERGENT DIVERGENT NOZZLE. JOURNAL OF SOLID AND FLUID MECHANICS[Internet]. 2017;7(1 ):101-112. Available from: https://sid.ir/paper/212710/en

    IEEE: Copy

    R. KAMALI, S.M. MOUSAVI, P. HOUSHYARI, and A. KHANEH ZAR, “NUMERICAL AND ANALYTICAL INVESTIGATION OF SHOCK TRAIN IN A CONVERGENT DIVERGENT NOZZLE,” JOURNAL OF SOLID AND FLUID MECHANICS, vol. 7, no. 1 , pp. 101–112, 2017, [Online]. Available: https://sid.ir/paper/212710/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button