| Citation: | YUAN Xiang-jiang, LI Guo-liang, LIU Zhi-yong, TU Guo-hua. Study of the instability characteristic in the boundary layer of a hypersonic blunt cone at low angle of attack[J]. Journal of Aerospace Power, 2011, 26(12): 2805-2811. |
| [1] |
Anderson J D.Hypersonic and high-temperature gas dynamics[M].Virgina:McGraw-Hill Companies,1989.
|
| [2] |
ZHONG X L,MA Y B.Boundary-layer receptivity of Mach 7.99 flow over a blunt cone to free-stream acoustic waves[J].Journal of Fluid Mechanics,2006,556:55-103.
|
| [3] |
Beckwith I E,Creel T R Jr.,Chen F J.Freestream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel[R].NASA Technical Paper 2180,1983.
|
| [4] |
Stetson K F,Thompson E R,Donaldson J,et al.On hypersonic transition testing and prediction[R].AIAA Paper 88-2007,1988.
|
| [5] |
Schneider S P,Matsumura S,Rufer S.Hypersonic stability and transition experiments on blunt cones and a generic scramjet forebody[R].AIAA Paper 2003-1130,2003.
|
| [6] |
李新亮,傅徳薰,马延文.可压缩尖锥边界层湍流的直接数值模拟[J].中国科学G辑,2008,38(1):89-101. LI Xinliang,FU Dexun,MA Yanwen.DNS of compressible turbulent boundary layer around a sharp cone[J].Science in China G,2008,8(1):89-101.(in Chinese)
|
| [7] |
苏彩虹,周恒.小攻角高超音速尖锥边界层的转捩预测和e-N法的改进[J].中国科学G辑,2009,39(1):123-130. SU Caihong,ZHOU Heng.The transition prediction of boundary layers on a hypersonic cone at small angle of attack and the improvement of the e-N method[J].Science in China G,2009,39(1):123-130.(in Chinese)
|
| [8] |
TU Guohuai,YUAN Xiangjiang.A characteristic-based shock-capturing scheme for hyperbolic problems[J].Journal of Computational Physics,2007,225(2):2083-2097.
|
| [9] |
Malik M,Balakumar P.Instability and transition in three-dimensional supersonic boundary layers[R].AIAA-92-5049,1992.
|
| [10] |
DiCristina V.Three-dimensional laminar boundary-layer transition on a sharp 8? cone at Mach 10[J].AIAA Journal,1970,8(5):852-856.
|
| [11] |
袁湘江,周恒.考虑流向曲率和压力梯度的可压缩边界层稳定性分析[J].空气动力学学报,1998,16(3):276-281. YUAN Xiangjiang,ZHOU Heng.Stability of compressible boundary layers with streamwise curvature and pressure grads[J].ACTA Aerodynamics Sinica,1998,16(3):276-281.(in Chinese)
|
| [12] |
Balakumar P,Jeyasingham S.Evolution of disturbances in three-dimensional boundary layers[R].AIAA-2000-014,2000.
|