Abstract
A two dimensional numerical simulation based on finite-volume method is performed to investigate the ramp-induced oblique detonation wave(ODW)’s interaction with a boundary layer, giving some details of this phenomenon. A comparison among cases which include inviscid-model ODW, viscous-model ODW and inert shock wave, all induced by a ramp, well shows the effect of boundary layer on the ODW, as well as the difference between ODW-boundary-layer interaction and shock-wave-boundary-layer interaction. The separation region of the boundary layer ahead of the ramp induced by the ODW is much larger than by the corresponding shock wave. Furthermore, as the separation region extends upstream, the effective angle of the ramp decreases for the ODW. As a result, the ramp cannot hold the ODW just at its tip. Instead, the ODW now stands at the rear of the ramp, likely to be a self-sustained detonation rather than an overdriven one.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Valorani, M., Di Giacinto, M., Buongiorno, C.: Performance prediction for oblique detonation wave engines(ODWE). Acta Astronautica 48(4), 211–228 (2001)
Fusina, G.: Numerical investigation of oblique detonation waves for shcramjet combustor. University of Toronto, Toronto (2003)
Miltiadis: A numerical study of wedge-induced detonations. Combustion and Flame 120, 526–538 (2000)
Pimentel, Azevedo, Figueira da Silva, et al.: Numerical study of wedge supported oblique shock wave-oblique detonation wave transitions. J. of the Braz. Soc, Mechanical Sciences XXIV, 149–157 (2002)
Choi, J.Y., Kim, D.W., In-Seuck, J., et al.: Cell-like structure of unstable oblique detonation wave from high-resolution numerical simulation. Proceedings of the Combustion Institute 31(2), 2473–2480 (2007)
Dudebout, R., Sislian, J.P., Oppitz, R.: Numerical simulation of hypersonic shock-induced combustion ramjets. Journal of Propulsion and Power 14(6), 869–879 (1998)
Xu, H., Jin, Z., Zhiyong, L., Shijie, L.: Initiation mechanism investigation of saltation and smoothness oblique detonation waves. Journal of Aerospace Power 27(12), 2674–2680 (2012)
Gui, M., Fan, B.: Wavelet Structure of Wedge-induced Oblique Detonation Waves. Combust. Sci. Technol 184, 1456–1470 (2012)
Teng, H., Jiang, Z.: On the transition pattern of the oblique detonation structure. J. Fluid Mech. 713, 659–669 (2012)
Choi, J.Y., In-Seuck, J., Youngbin, Y.: Scaling effect of the combustion induced by shock-wave boundary-layer interaction in premixed gas. In: Twenty-Seventh Sympostum(International) on Combustion/The Combustion Institute, pp. 2181–2188 (1998)
Kerimberkov, R.M., Ruban, A.I., Walker, I.D.A.: Hypersonic boundary layer separation on a cold wall. Journal of Fluid Mechanics (89), 535–552 (1978)
Hassaini, M.V., Baldwin, B.S., MacCormack, R.W.: Asymptotic features of shock wave boundary layer interaction. AIAA Journal 8(18), 1014–1016 (1980)
Lee, S., Loth, E., Wang, C.: LES of Supersonic Turbulent Boundary Layers with μVG’s. AIAA 2007-3916 (2007)
Anderson, B.H., Tinapple, J., Surber, L.: Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation. AIAA 2006-3197 (2006)
Hirt, S., Anderson, B.: Application of Micro-ramp Flow Control Devices to an Oblique Shock Interaction. AIAA (2008)
Babinsky, H., Li, Y., Ford, C.W.P.: Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions. AIAA JOURNAL 47(3), 668–675 (2009)
Anderson, J.D.: Computational Fluid Dynamics: The Basis with Applications. Mcgraw-Hill (1994)
Connaire, M.O., Curran, H.J., Simmie, J.M., Pitz, W.J., et al.: A comprehensive modeling study of hydrogen oxidation. International Journal of Chemical Kinetics 36(11), 603–622 (2004)
Menter, F.R.: Two-Equation Eddy-Viscorsity Turbulence Models for Engineering Applications. AIAA Journal 32(8), 1598–1605 (1994)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2014 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Liu, Y., Han, X., Lin, Z., Zhou, J. (2014). Numerical Study on Interaction of Ramp-Induced Oblique Detonation Wave with a Boundary Layer . In: Li, K., Xiao, Z., Wang, Y., Du, J., Li, K. (eds) Parallel Computational Fluid Dynamics. ParCFD 2013. Communications in Computer and Information Science, vol 405. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-53962-6_45
Download citation
DOI: https://doi.org/10.1007/978-3-642-53962-6_45
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-53961-9
Online ISBN: 978-3-642-53962-6
eBook Packages: Computer ScienceComputer Science (R0)