Article or book title, author's surname, DOI

Ignition of Supersonic Propane Air Flows Initiated by the Direct Current Discharge: Experiment and Numerical Modelling

N.E. Afonina1, V.G. Gromov2, A.P. Ershov3, S. Kamenshikov4, V.A. Chernikov5

research article Pages: 835-845

  1. 1 к. ф.-м. н., ст. научн. сотр., Институт механики МГУ им. М.В. Ломоносова
  2. 2 к. ф.-м. н., доцент, вед. научн. сотр., Институт механики МГУ им. М.В. Ломоносова
  3. 3 д. ф.-м. н., проф
  4. 4 мл. научн. сотр., Физический факультет МГУ им. М.В. Ломоносова
  5. 5 к. ф.-м. н., доцент, физический факультет МГУ им. М.В. Ломоносова

Abstract

Two types of inflammation, realized by cross - longitudinal arc discharge were investigated. Mutual influence of flow and flame led to formation of straight shock or shocks combination in front of heat supplier in one of two mentioned regimes. In its turn formation of shocks led to flow slowdown, pressure and temperature increase. Conditions for mixture ignition varied and we got unstable pulsed inflammation. It was experimentally achieved and analyzed. Inflammation was followed by sharp peak of pressure that was shock. It shifts stoichiometry point and stops plasma inflammation. As consequence we had a combination of inflammation and combustion pulses, followed by shocks. Ignition process existence was verified by spectral OH luminescence and integral luminescence obtained from the photo-amplifier. Exact correlation with pressure detectors was observed. In other area of electric parameters we could observe stable non-self-maintained inflammation of the propane -air mixture, which continued during the whole time of the discharge existence. It was confirmed by photo-amplifier data. Obtained results show that existence time of the discovered inflammation mode is (0.6 - 1 s). It is 6 times greater than duration of stationary flow establishment. That-s why described regime can be characterized as stationary non-self-maintained combustion of the high-speed propane-air mixture. High speed video measurements have shown space character of inflammation and further combustion wave. Streamer propagation is realized in complicated tracks that reflect turbulent structure of flow. In such a way integral area of energy input is three dimensional one and occupies 50% of channel section. Structure of streamers repeats form of reverse stream in area of step disposition. Numerical modeling verified appearance of quasi bounds in front of plasma and described parameters of flow close to that, found experimentally. Nevertheless model should include non thermal plasma mechanisms of inflammation and gas dynamic conditions of discharge.

How to cite

Афонина Н.Е., Громов В.Г., Ершов А.П., Каменщиков С.А., Черников В.А. Горение высокоскоростного воздушно-пропанового потока, инициируемое разрядом постоянного тока: эксперимент и численное моделирование // Нелинейный мир. 2009. № 11. С. 835–845.

References
  1. Bityurin V., Leonov S., Yarantsev D., VanWie D. Hydrocarbon Fuel Ignition by Electric Discharge in High-Speed Flow // Proc. 4th Workshop on Magnetoplasma Aerodynamics for Aerospace Applications. M.: IVTAN. 2002. P. 200.
  2. Jacobsen L. S., Carter C. D., Baurle R. A., et al. Toward Plasma-Assisted Ignition in Scramjets // Тр. III Междунар. симп.
    «Термохимические и плазменные процессы в аэродинамике». СПб. 28-31июля, 2003. С. 103.
  3. Klimov A., Bityurin V., Tolkunov B. et al. Non-Premixed Plasma-Assisted Combustion in High-Speed Airflow // AIAA. 2005.
    P. 2005-599.
  4. Esakov I., Grachev L., Khodataev K., Van Wie D. Efficiency of Microwave Discharges for Propane Ignition in Cold High-Speed Airflows // AIAA. 2005. P. 2005-989.
  5. Starikovskaia S., Kosarev I., Krasnochub A. et al.Control of Combustion and Ignition of Hydrocarbon-Containing Mixtures by
    Nanosecond Discharges  //AIAA. 2005. P. 2005-1195.
  6. Ершов А. П., Колесников Е. Б., Логунов А. А., Черников В. А. Параметры электродных разрядов в сверхзвуковых потоках воздуха // ТВТ. 2009. Т. 47. № 1.
  7. Ершов А. П., Сурконт О. С., Тимофеев И. Б. и др. Импульсные электрические разряды в сверхзвуковых потоках газа //
    Нелинейный мир. 2005. Т. 3. №1-2. C. 54-59.
  8. Ardelyan N.V., Ershov A.P., Chuvashev S.N., et al.Discharge and flame plasmas probe diagnostics in supersonic air-propane flows // AIAA. 2004. P. 2004-1016.
  9. Александров А.Ф., Ершов А.П., Логунов А.А.и др. Воспламенение сверхзвукового потока пропан-воздушной смеси электрическим разрядом // Вестник Московского Университета. Серия 3. Физика. Астрономия. 2008. Т. 49. № 1. С.78-80.
  10. Afonina N.E., Gromov V.G., Sakharov V.I. HIGHTEMP Technique for High Temperature Gas Flows Numerical Simulation. Proc. of the 5th European Symposium on Aerothermodynamics for Space Vehicles. Cologne. Germany. 8-11 November 2004. SP-563, February 2005. Р. 323-328
  11. Громов В. Г., Ершов А. П. , Левин В. А. , Шибков В. М. . Поперечные электрические  разряды в сверхзвуковых потоках воздуха. Моделирование эффектов, влияющих на нагрев газа в разрядном канале // ТВТ. 2006. № 2. Т. 44. С. 185-194.