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Temperature measurement in the PMMA k-phase during combustion in a high enthalpy flowunder the electrostatic field influence

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The purpose of present work is to clarify the mechanisms of the electrostatic field influence on the polymers (PMMA) combustion in high enthalpy flows. For this, the PMMA temperature profiles during combustion in a hybrid rocket engine studies were carried out. Based on the results obtained the assumption about the intensification of the substance entrainment from the polymer surface combusting in a high-enthalpy flow under the electrostatic field influence is confirmed.
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Journal of Physics: Conference Series
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Temperature measurement in the PMMA k-phase during combustion in
a high enthalpy flowunder the electrostatic field influence
To cite this article: I A Zyryanov et al 2020 J. Phys.: Conf. Ser. 1588 012019
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LTP Coatings 2019
Journal of Physics: Conference Series 1588 (2020) 012019
IOP Publishing
doi:10.1088/1742-6596/1588/1/012019
1
Temperature measurement in the PMMA k-phase during
combustion in a high enthalpy flowunder the electrostatic field
influence
I A Zyryanov1, A P Pozolotin1, A G Budin1
1 Vyatka State University, Department of Engineering Physics , 610000, Kirov,
Moskowskaya Street, 36, Russia
b185@mail.ru
Abstract. The purpose of present work is to clarify the mechanisms of the electrostatic field
influence on the polymers (PMMA) combustion in high enthalpy flows. For this, the PMMA
temperature profiles during combustion in a hybrid rocket engine studies were carried out.
Based on the results obtained the assumption about the intensification of the substance
entrainment from the polymer surface combusting in a high-enthalpy flow under the
electrostatic field influence is confirmed.
1. Introduction
The mechanism investigation of the electrostatic field influence on the polymers combustion in a high
enthalpy flow is important because the lack of knowledge in this area reduces the practical application
of electric fields as a tool for power plants controlling possibilities.
The background of these possibilities is shown in the articles [1-2], where the polymer (PMMA)
combustion process in the model hybrid rocket engine intensification with an electrostatic field was
demonstrated. The combustion rate was increased by 30% and the thrust increasedby 15%. It’s known
[3] possible processes explaining PMMA combustion intensification. The most interesting process
among them is number of nucleation (gasification) centers change during volumetric pyrolysis [2]. As
experimental data show, the number of gasification centers increases by an average by 30% under the
electrostatic field influence with a 5 kV potential difference. This leads to the substance dispersion
from the surface intensification, which manifests itself in the combustion rate increasing. This work
task is to clarify the field effect mechanism on combustion processes in the high enthalpy flow,
therefore, temperature measurements and the temperature gradients in the polymer changes estimation
were carried out.
2. Experiment Procedure
For experiments, a bench with a model hybrid rocket engine is used [1]. Temperature measurements
are made by chromel-alumel thermocouples with a junction diameter of 60 μm. The PMMA fuel block
is cut across, thermocouples are installed at the cut point at specified distances from the combustion
surface, then the halves of the block are glued together with dichloroethane. Thermo-EMF is recorded
by an analog millivoltmeter in order to minimize the electrostatic field effect on the thermocouple
readings. The error of temperature measurement does not exceed 10 0C.
LTP Coatings 2019
Journal of Physics: Conference Series 1588 (2020) 012019
IOP Publishing
doi:10.1088/1742-6596/1588/1/012019
2
3. Experimental Results
TheFig. 1 contains temperature over time graphs with an oxidizer consumption of 30.6 kg/m2, a block
length of 200 mm, combustion channel initial diameter of 20 mm and a voltage between electrodes of
0 and 5 kV are presented.
The shape of the curve at U = 0 kV is in qualitative agreement with the data of [4]. According to
[5], the PMMA thermal decomposition start temperature is in the range [150-200] 0C. The Fig. 1
contains inhomogeneities are observed in this temperature range, which arise due to thermocouple
junction contact with the gas bubbles in the subsurface of the polymer. It was not possible to
determine the exact value of the temperature at which the thermocouple exits to the surface, however,
in the literature [4-5], the possible value lies in the range [380-450] 0С.
Figure 1.Temperature vs. time.
In order to determine the electrostatic field influence features on the temperature distribution in the
PMMA k-phase, the temperature gradient was calculated for various oxidizing agent flow rate values
in the presence of field and without it. Fig. 2 shows graphs of the calculated gradients depending on
the temperature value; the legend shows the oxidizer consumption in kg/(m2s).The letter U at the flow
rate indicates the presence of an external field in the combustion zone.
LTP Coatings 2019
Journal of Physics: Conference Series 1588 (2020) 012019
IOP Publishing
doi:10.1088/1742-6596/1588/1/012019
3
Figure 2.Temperature gradient vs. temperature.
4. Discussion of results
It can be seen that with gas flow rate increasing the temperature gradient also increases. At the same
time, the electric field application decreases the gradient. Given the fact that the heat transfer byheat
conductivity between the flame and the polymer surface is 90% of the total heat flux [5], the reduction
of the temperature gradient in the fuel shows the decrease of the heat flux following deep into the
polymer under the electrostatic field.This could be due to the surface processes of gas formation and
dispersion intensification by an electrostatic field [6].As a result much more heat is carried away from
the fuel surface in the field presence.
During combustion, part of the heat is transferred by radiation. According to [5], the heat flux
radiant component goes to the PMMA decomposition with the bubbles formation in the entire heated
layer volume. The electric field effect leads to the fuel decomposition constants change [78].It
increases the number of bubbles in the surface layer. Hence this increases the thermal radiation
absorption on the surface, reducing the temperature gradient as well.
5. Conclusion
Thus, the paper presents the temperature measuring in the polymer during combustion in a high
enthalpy stream results.It is shown that under the electrostatic field influence, the temperature gradient
in polymer decreases.An explanation of the detected effects is proposed.
References
[1] Reshetnikov S M, Zyryanov I A, Pozolotin A P and Budin A G Electrostatic field influence on
the combustion rate in hybrid rocket 2015 Vestnik of the Kazan State Technical University
71 52-7
[2] Reshetnikov S M, Zyryanov I A, Budin A G and Reshetnikov I S Hybrid rocket engine control
by the electrostatic field 2018 Journal of Engineering Science and Technology Review 11
146-50
[3] Zyryanov I A, Reshetnikov S M, Budin A G, Pozolotin A P and Shaurko P N To the question
of combustion modeling in a HRE under electric field influence 2016 Society, Science,
Innovation (NPK - 2016): collection of articles / Vyatka State University 1740-5
LTP Coatings 2019
Journal of Physics: Conference Series 1588 (2020) 012019
IOP Publishing
doi:10.1088/1742-6596/1588/1/012019
4
[4] Contadin S, Conte A, Karp A C, Jens E T, Vaughan D and Pastrone D G Thermal analysis of a
hybrid rocket propulsion system for interplanetary CubeSats 2017 7th European Conference
for Aeronautics and Aerospace Sciences (EUCASS)
[5] Reshetnikov S M and Reshetnikov I S 2014 Combustion Anathomy (Moscow: NGSS) p 247
[6] Reshetnikov S M, Zyryanov I A, Budin A G and Pozolotin A P High temperature
polymethylmethacrylate decomposition in the electrostatic field features 2016 Vestnik of the
Kazan Technological University 19
[7] Laptenko B K The electrostatic field effect on the low temperature decomposition of
ammonium perchlorate 1977 Combustion Physics and Methods of its Research 7 71-4
[8] Kishore K, Paiverneker V R and Sunitha M R Influence of the electric field on the low
temperature thermal decomposition of ammonium perchlorate/plystyrene propellant 1982
Combustion and Flame 3 1-6
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Full-text available
Design of the effective hybrid rocket engines requires development of adequate control methods for the condensed phase regression rates. There are two traditional approaches: prescription with catalytic additives and geometrical with oxidizer flux involution or burning channel profiling. Other methods are significantly less investigated, including using various fields for the combustion process control. The paper presents some experimental results on the influence of electrostatic field on the combustion rate for the PMMA - gaseous oxygen hybrid fuel engine. It was shown that it is possible to control engine thrust with parameters of the control field. Some analysis and model explanations are performed.
To the question of combustion modeling in a HRE under electric field influence
  • I A Zyryanov
  • S M Reshetnikov
  • A G Budin
  • A Pozolotin
  • P N Shaurko
Zyryanov I A, Reshetnikov S M, Budin A G, Pozolotin A P and Shaurko P N To the question of combustion modeling in a HRE under electric field influence 2016 Society, Science, Innovation (NPK -2016): collection of articles / Vyatka State University 1740-5
To the question of combustion modeling in a HRE under electric field influence 2016
  • Zyryanov
High temperature polymethylmethacrylate decomposition in the electrostatic field features 2016
  • Reshetnikov
Electrostatic field influence on the combustion rate in hybrid rocket 2015
  • Reshetnikov
The electrostatic field effect on the low temperature decomposition of ammonium perchlorate 1977
  • Laptenko