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:

1,154
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

EXPERIMENTAL STUDY OF COMBUSTION INSTABILITY IN PREMIXED GAS TURBINE ENGINES

Pages

  1-13

Abstract

 Lean premixed combustion is widely used in recent years as a method to achieve the environmental standards with regard to NOx emission. In spite of the advantages, premixed combustion systems with equivalence ratios less than one are susceptible to COMBUSTION INSTABILITY. To study the lean COMBUSTION INSTABILITY experimentally, one premixed combustion setup, equipped with reactant supplying system, is designed and manufactured. In this research, gaseous propane is introduced as fuel and experiments are performed at nearly atmospheric pressure with equivalence ratios within the range of 0.7 to 1.5 and fuel mass flow rates of 2 to 4 gr/s. It has been observed that the combustion chamber of the gas turbine becomes unstable when equivalence ratio is less than one. To distinguish the COMBUSTION INSTABILITY, through various operating conditions, probability density functions, spectral diagrams, space distribution of pressure oscillations, along with Rayleigh criteria are employed. Accordingly, equivalence ratio effects in stabilizing the unstable combustion system are investigated experimentally. Moreover, convective delay time is calculated for all experiments and the results are compared with Rayleigh Criteria, showing relatively good agreements. Finally, stability limits are identified, based on inlet mass flow rate and equivalence ratio.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    AKBARI, NOUZAR, SERAJ MAHDIZADEH, N., & EBRAHIMI, REZA. (2009). EXPERIMENTAL STUDY OF COMBUSTION INSTABILITY IN PREMIXED GAS TURBINE ENGINES. AEROSPACE MECHANICS JOURNAL, 4(4 (14)), 1-13. SID. https://sid.ir/paper/101852/en

    Vancouver: Copy

    AKBARI NOUZAR, SERAJ MAHDIZADEH N., EBRAHIMI REZA. EXPERIMENTAL STUDY OF COMBUSTION INSTABILITY IN PREMIXED GAS TURBINE ENGINES. AEROSPACE MECHANICS JOURNAL[Internet]. 2009;4(4 (14)):1-13. Available from: https://sid.ir/paper/101852/en

    IEEE: Copy

    NOUZAR AKBARI, N. SERAJ MAHDIZADEH, and REZA EBRAHIMI, “EXPERIMENTAL STUDY OF COMBUSTION INSTABILITY IN PREMIXED GAS TURBINE ENGINES,” AEROSPACE MECHANICS JOURNAL, vol. 4, no. 4 (14), pp. 1–13, 2009, [Online]. Available: https://sid.ir/paper/101852/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
    File Not Exists.
    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