i-manager Publications

Optimization of Pintle Injector Position to Control Thrust Propulsion

Phanibhaskar Anusuri*, Akella Yeswanth**, Raghuveer Nemani***

*-*** Department of Mechanical Engineering, Pragati Engineering College, Surampalem, India.

Periodicity:November - January'2022
DOI : https://doi.org/10.26634/jme.12.1.18267

Abstract

Pintle nozzle plays a pivotal role in the field of aerospace industry because of the feature of controlling thrust propulsion and steering. The peculiar nozzle design of the pintle injector helps in proper mixing of propellants and also forces fluids into the combustion chamber. The position of pintle in rocketry nozzle also contributes in improving efficiency. This paper is concerned to perform CFD analysis to optimize shape of the pintle head and also by varying different positions of the pointer or pintle. In the later stage the results are tabulated for two different speeds of flow namely Minimum and Maximum. The graphs were plotted for Static Pressure, Velocity Magnitude, Turbulent Kinetic Energy, Cell Reynolds number and Strain Rate and best model is assessed. The total study and simulation was performed using ANSYS Fluent 14.5.

Keywords

Propulsion, Pintle, Nozzle.

How to Cite this Article?

Anusuri, P., Yeswanth, A., and Nemani, R. (2022). Optimization of Pintle Injector Position to Control Thrust Propulsion. i-manager’s Journal on Mechanical Engineering, 12(1), 6-12. https://doi.org/10.26634/jme.12.1.18267

References

[1]. Belega, B. A., & Nguyen, T. D. (2015, May). Analysis of flow in convergent-divergent rocket engine nozzle using computational fluid dynamics. In International Conference of Scientific Paper (Vol. 6), pp. 1-6.

[2]. Dressler, G., & Bauer, J. (2000, July). TRW pintle engine heritage and performance characteristics. In 36^th AiAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1-22. https://doi.org/10.2514/6.2000-3871

[3]. Gaur, D., & Prakash, O. (2018). Comparative Viscous Flow Analysis for Rocket Engine Convergent-Divergent Nozzle for Distinct Geometric Parameters. International Journal of Innovative Research in Science, Engineering and Technology, 7(6), 7476-7483. https://doi.org/10.156 80/IJIRSET.2018.0706118

[4]. Kumar, P. V., & Kumar, B. K. (2017). Design and CFD Analysis of Convergent and Divergent Nozzle. International Journal of Professional Engineering Studies, 9(2), 150-163.

[5]. Murugan, N., Saravanan, V., Doddi, H. N., Nejaamtheen, M. N., Kumar, V. R. S., & Murugesh, P. (2017). Conceptual design and shape optimization of a pintle nozzle for controllable thrust propulsion and steering in: 53^rd AIAA. In SAE/ASEE Joint Propulsion Conference. 1-21. https://doi.org/10.2514/6.2017-4870

[6]. Narayana, K. P. S. S., & Reddy, K. S. (2016). Simulation of convergent divergent rocket nozzle using CFD analysis. IOSR Journal of Mechanical and Civil Engineering, 13(4), 58-65. https://doi.org/10.9790/1684-1304015865

[7]. Patil, P. V., More, A. A., Patil, S. M., & Mokal, M. R. (2017). Optimization In DE-Laval Nozzle Design to Increase Thrust, International Journal of Scientific & Engineering Research, 8(3), 81-84.

[8]. Prathibha, M., Gupta, M. S., & Naidu, S. (2015). CFD Analysis on a Different Advanced Rocket Nozzles. International Journal of Engineering and Advanced Technology, 4(6), 14-22.

[9]. Roy, P., Mondal, A., & Barai, B. (2016). CFD Analysis of Rocket Engine Nozzle. International Journal of Advanced Engineering Research and Science, 3(1), 39-46.

[10]. Sreenath, K. R., & Mubarak, A. K. (2016). Design and analysis of contour bell nozzle and comparison with dual bell nozzle. International Journal of Research and Engineering, 3(6), 52-56.

	North Americas,UK, Middle East,Europe		India	Rest of world
	USD	EUR	INR	USD-ROW
Pdf	35	35	200	20
Online	35	35	200	15
Pdf & Online	35	35	400	25

Optimization of Pintle Injector Position to Control Thrust Propulsion

Abstract

Keywords

How to Cite this Article?

References

If you have access to this article please login to view the article or kindly login to purchase the article

Purchase Instant Access

Options for accessing this content: