Quasi-One-Dimensional Numerical Method for Solid Fuel Scramjet Combustor Analysis and Design
Publication: Journal of Aerospace Engineering
Volume 28, Issue 3
Abstract
To research the performance of a solid fuel scramjet combustor, a solid fuel regression rate model was coupled into a quasi-one-dimensional flow equation, and so the flow parameters and fuel regression rate could be calculated together. According to the regression rate and the combustor diameter in the previous moment, the combustor diameter of the next moment could be obtained. The unsteady combustion and flow matter in the combustor was simplified into a steady calculation of every moment by solving the boundary condition at different moments independently. The numerical results were compared to actual experimental data from the literature, and they agreed well with the experiment. Taking the fuel/air ratio and Mach number as the optimization conditions, the initial size of the combustor could be obtained. On the basis of an optimized combustor, the relevant parameters’ variation rules were calculated and analyzed. It was found that during the working process, the combustor flow field could be kept at the supersonic flow state, the axial fuel regression rate at a specific moment first increases and then tends to be steady, the local fuel regression rate at a specific position decreases gradually with time, the mass flow rate at the combustor exit and the fuel/air ratio is relatively steady, and the total pressure recovery coefficient and the specific impulse of the combustor decline gradually.
Get full access to this article
View all available purchase options and get full access to this article.
Acknowledgments
This study was supported by the National Natural Science Foundation of China (Grant 51276020).
References
Angus, W. J. (1991). “An investigation into the performance characteristics of a solid fuel scramjet propulsion device.” M.S. thesis, Naval Postgraduate School, Monterey, CA.
Angus, W. J., Witt, M. A., Laredo, D., and Netzer, D. W. (1993). “Solid fuel supersonic combustion.” La Recherche Aerospatiale, 6, 1–8.
Ben-Arosh, R., Natan, B., Spiegler, E., and Gany, A. (1999). “Theoretical study of a solid fuel scramjet combustor.” Acta Astronaut., 45(3), 155–166.
Ben-Yakar, A. (1995). “Investigation of the combustion of solid fuel at supersonic conditions in a ramjet engine.” M.S. thesis, Technion—Israel Institute of Technology, Haifa, Israel.
Ben-Yakar, A., and Gany, A. (1994). “Experimental study of a solid fuel scramjet.” Proc., 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conf., AIAA, Washington, DC.
Ben-Yakar, A., Natan, B., and Gany, A. (1998). “Investigation of a solid fuel scramjet combustor.” J. Propul. Power, 14(4), 447–455.
Cohen-Zur, A., and Natan, B. (1998). “Experimental investigation of a supersonic combustion solid fuel ramjet.” J. Propul. Power, 14(6), 880–889.
Jarymowycz, T. A., Yang, V., and Kuo, K. (1992). “Numerical study of solid-fuel combustion under supersonic crossflows.” J. Propul. Power, 8(2), 346–353.
Saraf, S., and Gany, A. (2007). “Testing metallized solid fuel scramjet combustor.” Proc., Int. Symp. of Air Breathing Engine (ISABE2007), AIAA, Reston, VA.
Simone, D., and Bruno, C. (2009). “LiH as fuel for solid fuelled scramjet engines.” Proc., 47th AIAA 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA, Washington, DC.
Uenishi, K., Rogers, R. C., and Northamt, G. B. (1989). “Numerical predictions of a rearward-facing-step flow in a supersonic combustor.” J. Propul. Power, 5(2), 158–164.
Wilde, J. (1991). “Fuel pyrolysis effects on hybrid rocket and solid fuel ramjet combustor performance.” Ph.D. thesis, Delft Univ. of Technology, Delft, Netherlands.
Witt, M. A. (1989). “Investigation into the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles.” M.S. thesis, Naval Postgraduate School, Monterey, CA.
Information & Authors
Information
Published In
Copyright
© 2014 American Society of Civil Engineers.
History
Received: Aug 28, 2013
Accepted: Dec 25, 2013
Published online: Dec 27, 2013
Discussion open until: Dec 17, 2014
Published in print: May 1, 2015
Authors
Metrics & Citations
Metrics
Citations
Download citation
If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.