Numerical Study of Hypersonic Glide Vehicle based on Blunted Waverider
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.
[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
[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
@article{"International Journal of Mechanical, Industrial and Aerospace Sciences:54773", author = "Liu Jian-xia and Hou Zhong-xi and Chen Xiao-qing", title = "Numerical Study of Hypersonic Glide Vehicle based on Blunted Waverider", abstract = "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", volume = "5", number = "7", pages = "1310-6", }
