Citation: | WANG J Q,CHEN Z,NI Z Y,et al. Experimental study on structural characteristics of separation flow induced by 3D wedge in hypersonic laminar flow by oil visualization[J]. Journal of Experiments in Fluid Mechanics, 2021,35(5):115-120. doi: 10.11729/syltlx20180026 |
[1] |
LEWIS J E,KUBOTA T,LEES L. Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling[J]. AIAA Journal,1968,6(1):7-14. doi: 10.2514/3.4434
|
[2] |
HOLDEN M S. Shock wave-turbulent boundary layer interaction in hypersonic flow[C]//Proc of the 10th Aerospace Sciences Meeting. 1977. doi: 10.2514/6.1972-74
|
[3] |
MALLINSON S G,GAI S L,MUDFORD N R. The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects[J]. Journal of Fluid Mechanics,1997,342:1-35. doi: 10.1017/s0022112097005673
|
[4] |
LI S X, CHEN Y K. A study of interaction flow induced by 3D wedge[C]// Proceeding of the 3rd International Conference Fluid-Mechanics. 1997.
|
[5] |
CANDLER G, NOMPELIS I, HOLDEN M S. Computational analysis of hypersonic laminar viscous-inviscid interactions[R]. AIAA-2000-0532, 2000. doi: 10.2514/6.2000-532
|
[6] |
DOLLING D S. Fifty years of shock-wave/boundary-layer interaction research: What next?[J]. AIAA Journal,2001,39(8):1517-1531. doi: 10.2514/2.1476
|
[7] |
BABINSKY H, HARVEY J K. Shock wave-boundary-layer interac-tions[M]. Cambridge: Cambridge University Press, 2011. doi: 10.1017/cbo9780511842757
|
[8] |
余平,段毅,尘军. 高超声速飞行的若干气动问题[J]. 航空学报,2015,36(1):7-23.
YU P,DUAN Y,CHEN J. Some aerodynamics issue in hypersonic flight[J]. Acta Aeronautica et Astronautica Sinica,2015,36(1):7-23.
|
[9] |
DRUGUET M C,CANDLER G V,NOMPELIS I. Effects of numerics on Navier-Stokes computations of hypersonic double-cone flows[J]. AIAA Journal,2005,43(3):616-623. doi: 10.2514/1.6190
|
[10] |
陈政, 倪招勇, 王军旗, 等. 高超声速层流分离流动模拟影响因素分析[C]// 全国第十五届分离流、旋涡和流动控制会议论文集. 2014.
|
[11] |
李艳丽,李素循. 高超声速绕钝舵层流干扰流场特性研究[J]. 宇航学报,2007,28(6):1472-1477. doi: 10.3321/j.issn:1000-1328.2007.06.007
LI Y L,LI S X. Investigation of interactive hypersonic laminar flow over blunt fin[J]. Journal of Astronautics,2007,28(6):1472-1477. doi: 10.3321/j.issn:1000-1328.2007.06.007
|
[12] |
PRINCE S, VANNAHME M, STOLLERY J. Experiments on the hypersonic turbulent shock-wave/boundary layer interaction and the effects of surface roughness[R]. AIAA-99-0147, 1999. doi: 10.2514/6.1999-147
|
[13] |
李素循,倪招勇. 高超声速层流干扰流场研究[J]. 宇航学报,2003,24(6):547-551, 573. doi: 10.3321/j.issn:1000-1328.2003.06.001
LI S X,NI Z Y. Investigation of laminar interactive flowfield in hypersonic flow[J]. Journal of Astronautics,2003,24(6):547-551, 573. doi: 10.3321/j.issn:1000-1328.2003.06.001
|
[14] |
INGER G R. Scaling of incipient separation in high speed laminar flows[J]. AIAA Journal,1995,33(1):178-181. doi: 10.2514/3.12356
|