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Numerical Study of Hypersonic Glide Vehicle based on Blunted Waverider

Authors: Liu Jian-xia, Hou Zhong-xi, Chen Xiao-qing


The waverider is proved to be a remarkably useful configuration for hypersonic glide vehicle (HGV) in terms of the high lift-to-drag ratio. Due to the severe aerodynamic heating and the processing technical restriction, the sharp leading edge of waverider should be blunted, and then the flow characteristics and the aerodynamic performance along the trajectory will change. In this paper, the flow characteristics of a HGV, including the rarefied gas effect and transition phenomenon, were studied based on a reference trajectory. A numerical simulation was carried out to study the performance of the HGV under a typical condition.

Keywords: Aerodynamic, CFD, Thermodynamic, Waverider

Digital Object Identifier (DOI):

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[1] Y. Sun, H. P. Zhao, "Application analysis and prospects of near-space vehicles," Signal and Information, vol. 138, no. 110, 2008, pp. 26-28.(in Chinese)
[2] R. T. Voland, L. D. Huebner, C. R. Mcclinton, "X-43A hypersonic vehicle technology development," Acta Astronautica, vol. 59, 2006, pp. 181-191.
[3] I. Dietlein, A. Kopp, "System analysis for ÔÇÿsharp-edge- re-entry vehicles," in 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009.
[4] Z. H. Qu, W. Liu, M. Zeng, J. Liu, "Hypersonic aerodynamics," NUDT press, 2001, pp. 206-222 (in Chinese)
[5] Z. H. Wang, L Bao, B. G. Tong, "Variation character of stagnation point heat flux for hypersonic pointed bodies from continuum to rarefied flow states and its bridge function study," Sci China Ser G, vol. 39, no. 8, 2009, pp. 1134-1140.
[6] R. L. Zhu, Y. H. Cao, " The hybrid code of adaptive local time step for DSMC PEPSM on the hypersonic vehicle," Acta Aerodynamica Sinica vol. 26, no. 3, 2009, pp. 394-399.
[7] V. V. Riabov, "Heat transfer on a hypersonic sphere with diffuse rarefied-gas injection," in 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2004.
[8] W. F. N. Santos, M. J. Lewis, "Aerodynamic heating performance of power law leading edges in rarefied hypersonic flow," in 36th AIAA Thermo physics Conference, Orlando, Florida, 2003.
[9] A. Jocksch, L. Kleiser, "Growth of turbulent spots in high-speed boundary layers on a flat plate," International Journal of Heat and Fluid Flow, vol. 29, 2008, pp. 1543-1557.
[10] E. Benard, R. K. Cooper, A. Sidorenko, "Transitional and turbulent heat transfer of swept cylinder attachment line in hypersonic flow," International Journal of Heat and Mass Transfer, vol. 49, 2006, pp. 836-843.
[11] S. P. Schneider, "Hypersonic laminar-turbulent transition on circular cones and scramjet forebodies," Progress in Aerospace Sciences, vol. 40, 2008, pp. 1-50.
[12] S. P. Schneider, "Flight data for boundary-layer transition at hypersonic and supersonic speeds," Journal of Spacecraft and Rockets, vol. 36, no. 1, 1999, pp. 8-20.
[13] N. Sheetz, "Ballistics range boundary layer transition measurements on cones at hypersonic speeds," Viscous Drag Reduction, 1968.
[14] D. O.Van mol, J. D. J. Anderson, "Heat transfer characteristics of hypersonic wave-riders with an emphasis on leading edge effects," AIAA92-2920.
[15] M. J.Lewis, M.Chauffour, "Shock-based waverider design with pressure gradient corrections and computational simulations," Journal of Aircraft, vol. 42, no. 15, 2005, pp. 1350-1352.
[16] Y. K. Wang, S. F. Yang, D. J. Zhang, X. Y. Deng. "Design of waverider configuration with high lift-drag ratio," Journal of Aircraft, vol. 44, no. 1, 2007, pp. 144-148.
[17] T. F. Zien, "Determination of surface pressure and temperature distributions on hypersonic waveriders," in 26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, 2008.
[18] J. Che, S. Tang, "Research on integrated optimization design of hypersonic cruise vehicle," Aerospace Science and Technology. vol. 12, 2008, pp. 567-572.
[19] C. M. Di, M. Marini, B. S. Di, A. Schettino, G. Ranuzzi. "Numerical prediction of aerothermodynamic effects on a reentry vehicle body flap configuration," Acta Astronautica. vol. 65, 2009, pp. 221-239.
[20] J. Pan, C. Yan, Y.F Geng, J. Wu, "Aerothermodynamics of the waveriders applying artificially blunted leading edge concept," in 47th AIAA Aerospace Sciences Meeting Including the New Horizons forum, Orlando, Florida, 2009.
[21] X. Liu, X. G. Deng. "Application of high-order accurate algorithm to hypersonic viscous flows for calculating heat transfer distributions," in 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada: 2007.
[22] K. H. Kim, C. Kim, O. Hyun. "Methods for the accurate computations of hypersonic flows I: AUSMPW+ scheme," Journal of Computational Physics, vol. 174, 2001, pp. 38-80.
[23] J. H. Lee, O. H. Rho., "Numerical analysis of hypersonic viscous flow around a blunt body using Roe-s FDS and AUSM+ schemes," AIAA paper 97-2054, 1997.
[24] R. Bur, B. Chanetz, "Experimental study on the PRE-X vehicle focusing on the transitional shock-wave/boundary-layer interactions," Aerospace Science and Technology, vol. 13, 2009, pp. 393-401.
[25] X. Q. Chen, "Research on aerodynamic design for hypersonic waverider vehicle," ChangSha, NUDT, 2006
[26] J. J. Bertin, R. M. Cummings, "Critical hypersonic aerothermodynamic phenomena," Annual Review of Fluid Mechanics, vol. 38, 2006, pp. 129-157
[27] J. X. Liu, "Modeling and analysis on aerodynamic heating for hypersonic glide vehicle," ChangSha, NUDT, 2008