Performance Enhancement of a Supersonic Air Intake by Applying a Heat Source
Publication: Journal of Aerospace Engineering
Volume 33, Issue 5
Abstract
The main objective of this paper is to study the effects of applying a heat source ahead of a supersonic mixed compression air intake. This intake has been designed for the freestream Mach number 2. Four parameters of the heat source, including its location, cross-sectional shape, cross-sectional area, and heat generation rate, are investigated numerically to find a suitable heat source that enhances the performance of the intake. The research is conducted at the freestream Mach numbers of 1.8, 2, and 2.2. Total pressure recovery, mass flow ratio, flow distortion, and drag coefficient are considered as the intake performance parameters. Variation of the critical backpressure is further investigated. The results show that a bow shock is formed around the heat source that affects the intake shock system and can have desirable effects on most of the performance parameters and the critical backpressure at different freestream Mach numbers. It is also observed that the heat source location is the most effective parameter of the heat source, and should be selected meticulously.
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Data Availability Statement
All data, models, and code generated or used during the study appear in the published article.
Acknowledgments
This study was financially supported by Ferdowsi University of Mashhad (FUM), Iran (Grant No. 46236).
References
Cai, C., and X. He. 2007. “Energy deposition/extraction effects on oblique shock waves over a wedge.” AIAA J. 45 (9): 2267–2272. https://doi.org/10.2514/1.28920.
Chang, J. T., W. Bao, D. Yu, Y. Fan, Y. Shen, and W. Zhou. 2009. “Hypersonic inlet control with pulse periodic energy addition.” Proc. Inst. Mech. Eng., Part G: J. Aerosp. Eng. 223 (6): 691–699.
Falempin, F., A. A. Firsov, D. A. Yarantsev, M. A. Goldfeld, K. Timofeev, and S. B. Leonov. 2015. “Plasma control of shock wave configuration in off-design mode of inlet.” Exp. Fluids 56 (3): 1–10. https://doi.org/10.1007/s00348-015-1928-4.
Ganiev, Y. C., V. P. Gordeev, A. V. Krasilnikov, V. I. Lagutin, V. N. Otmennikov, and A. V. Panasenko. 2000. “Aerodynamic drag reduction by plasma and hot-gas injection.” J. Thermophys. Heat Transfer 14 (1): 10–17. https://doi.org/10.2514/2.6504.
Georgievskii, P. Y., and V. A. Levin. 2003. “Control of the flow past bodies using localized energy addition to the supersonic oncoming flow.” Fluid Dyn. 38 (5): 794–805. https://doi.org/10.1023/B:FLUI.0000007841.91654.10.
Guvernyuk, S. V., and A. B. Samoilov. 1997. “Control of supersonic flow around bodies by means of a pulsed heat source.” Tech. Phys. Lett. 23 (5): 333–336. https://doi.org/10.1134/1.1261673.
Hafenrichter, E., Y. Lee, J. Dutton, and E. Loth. 2003. “Normal shock/boundary-layer interaction control using aeroelastic mesoflaps.” J. Propul. Power 19 (3): 464–472. https://doi.org/10.2514/2.6130.
Hill, P., and C. Peterson. 1992. Mechanics and thermodynamics of propulsion. 2nd ed. Boston: Addison-Wesley Longman.
Kandala, R., and G. V. Candler. 2004. “Numerical studies of laser-induced energy deposition for supersonic flow control.” AIAA J. 42 (11): 2266–2275. https://doi.org/10.2514/1.6817.
Karim, M., M. Rahman, and M. A. Alim. 2011. “Performance of SST turbulence model for computation of viscous drag of axisymmetric underwater bodies.” Int. J. Eng. 24 (2): 139–146.
Kim, S. 2009. “Aerodynamic design of a supersonic inlet with a parametric bump.” J. Aircr. 46 (1): 198–202. https://doi.org/10.2514/1.37416.
Kremeyer, K. 2004. “Lines of pulsed energy for supersonic/hypersonic drag reduction: Generation and implementation.” In Proc., 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reston, VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-984.
Kremeyer, K., K. Sebastian, and C. Shu. 2006. “Computational study of shock mitigation and drag reduction by pulsed energy lines.” AIAA J. 44 (8): 1720–1731. https://doi.org/10.2514/1.17854.
Li, Q., Y. Hong, W. Zhao, and D. Wang. 2014. “Numerical simulation on air mass capture control of hypersonic inlet by laser energy.” Proc., Appl. Mech. Mater. 644–650: 1470–1473.
Luk’yanov, G. A. 1998. “Drag and heat exchange of an object in a supersonic flow with a planar source of energy in front of the object.” Tech. Phys. Lett. 24 (12): 980–982. https://doi.org/10.1134/1.1262341.
Macheret, S. O., M. N. Shneider, and R. B. Miles. 2004. “Scramjet inlet control by off-body energy addition: A virtual cowl.” AIAA J. 42 (11): 2294–2302. https://doi.org/10.2514/1.3997.
Maru, Y., N. Tanatsugu, T. Sato, H. Kobayashi, T. Kojima, and K. Okai. 2004. “Multi-row disk arrangement concept for spike of axisymmetric air inlet.” In Proc., 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit. Fort Lauderdale, FL.
Masud, J., and F. Akram. 2010. “Flow field and performance analysis of an integrated diverterless supersonic inlet.” In Proc., 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-481.
McCormick, D. 1993. “Shock/boundary-layer interaction control with vortex generators and passive cavity.” AIAA J. 31 (1): 91–96. https://doi.org/10.2514/3.11323.
Menter, F. R. 1994. “Two-equation eddy-viscosity turbulence models for engineering applications.” AIAA J. 32 (8): 1598–1605. https://doi.org/10.2514/3.12149.
Oswatitsch, K. 1959. Propulsion with heating at supersonic speed. Berlin: Deutsche Versuchsanstalt fur Luft und Raumfahrt.
Reichert, B., and B. Wendt. 1996. “Improving curved subsonic diffuser performance with vortex generators.” AIAA J. 34 (1): 65–72. https://doi.org/10.2514/3.13022.
Seddon, J., and E. L. Goldsmith. 1999. Intake aerodynamics: AIAA education series. 2nd ed. Oxford, UK: Blackwell Science.
Sepahi-Younsi, J., and B. Forouzi Feshalami. 2019. “Performance evaluation of external and mixed compression supersonic air intakes: Parametric study.” J. Aerosp. Eng. 32 (5): 04019066. https://doi.org/10.1061/(ASCE)AS.1943-5525.0001048.
Soltani, M. R., A. Daliri, and J. Sepahi-Younsi. 2016. “Effects of shock wave/boundary-layer interaction on performance and stability of a mixed-compression inlet.” Sci. Iranica 23 (4): 1811–1825. https://doi.org/10.24200/sci.2016.3928.
Soltani, M. R., M. Farahani, and J. Sepahi-Younsi. 2011. “Performance study of a supersonic inlet in the presence of a heat source.” Sci. Iranica 18 (3): 375–382. https://doi.org/10.1016/j.scient.2011.05.027.
Soltani, M. R., and J. Sepahi-Younsi. 2016. “Buzz cycle description in an axisymmetric mixed-compression air intake.” AIAA J. 54 (3): 1040–1053. https://doi.org/10.2514/1.J054215.
Soltani, M. R., J. Sepahi-Younsi, and A. Daliri. 2014. “Performance investigation of a supersonic air intake in the presence of the boundary layer suction.” Proc. Inst. Mech. Eng., Part G: J. Aerosp. Eng. 229 (8): 1495–1509. https://doi.org/10.1177/0954410014554815.
Soltani, M. R., J. Sepahi-Younsi, and M. Farahani. 2012. “Investigation of a new flux scheme for the numerical simulation of the supersonic intake flow.” Proc. Inst. Mech. Eng., Part G: J. Aerosp. Eng. 226 (11): 1445–1454. https://doi.org/10.1177/0954410011422634.
Soltani, M. R., J. Sepahi-Younsi, and M. Farahani. 2013. “Numerical simulation and parametric study of a supersonic intake.” Proc. Inst. Mech. Eng., Part G: J. Aerosp. Eng. 227 (3): 467–479. https://doi.org/10.1177/0954410012436620.
Soltani, M. R., J. Sepahi-Younsi, and M. Farahani. 2015a. “Effects of boundary-layer bleed parameters on supersonic intake performance.” J. Propul. Power 31 (3): 826–836. https://doi.org/10.2514/1.B35461.
Soltani, M. R., J. Sepahi-Younsi, and V. F. Khanaposhtani. 2015b. “Numerical Investigation of the unstart suppression in a supersonic air intake.” Iranian J. Sci. Technol. 39 (M2): 413–426. https://doi.org/10.22099/ijstm.2015.3249.
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©2020 American Society of Civil Engineers.
History
Received: Aug 27, 2019
Accepted: Mar 9, 2020
Published online: May 30, 2020
Published in print: Sep 1, 2020
Discussion open until: Oct 30, 2020
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