Citation: | CHEN J F,XU Y,JIANG W Q,et al. Infrared thermogram measurement experiment of hypersonic boundary-layer transition of a lifting body[J]. Journal of Experiments in Fluid Mechanics. doi: 10.11729/syltlx20220030 |
[1] |
陈坚强, 涂国华, 张毅锋, 等. 高超声速边界层转捩研究现状与发展趋势[J]. 空气动力学学报, 2017, 35(3): 311–337.
CHEN J Q, TU G H, ZHANG Y F, et al. Hypersnonic boundary layer transition: what we know, where shall we go[J]. Acta Aerodynamica Sinica, 2017, 35(3): 311–337.
|
[2] |
段毅, 姚世勇, 李思怡, 等. 高超声速边界层转捩的若干问题及工程应用研究进展综述[J]. 空气动力学学报, 2020, 38(2): 391–403. doi: 10.7638/kqdlxxb-2020.0041
DUAN Y, YAO S Y, LI S Y, et al. Review of progress in some issues and engineering application of hypersonic bound-ary layer transition[J]. Acta Aerodynamica Sinica, 2020, 38(2): 391–403. doi: 10.7638/kqdlxxb-2020.0041
|
[3] |
孙杭义, 陈喜兰, 罗月培, 等. 高超声速飞行器边界层转捩飞行实验项目地面试验进展[J]. 飞航导弹, 2020(6): 23–28.
|
[4] |
李强, 赵磊, 陈苏宇, 等. 展向凹槽及泄流孔对高超声速平板边界层转捩影响的试验研究[J]. 物理学报, 2020, 69(2): 024703. doi: 10.7498/aps.69.20191155
LI Q, ZHAO L, CHEN S Y, et al. Experimental study on effect of transverse groove with/without discharge hole on hypersonic blunt flat-plate boundary layer transition[J]. Acta Physica Sinica, 2020, 69(2): 024703. doi: 10.7498/aps.69.20191155
|
[5] |
CASPER K M, BERESH S J, HENFLING J F, et al. Hypersonic wind-tunnel measurements of boundary-layer transition on a slender cone[J]. AIAA Journal, 2016, 54(4): 1250–1263. doi: 10.2514/1.J054033
|
[6] |
JULIANO T J, KIMMEL R L, WILLEMS S, et al. HIFiRE-1 boundary-layer transition: ground test results and stability analysis[C]//Proc of the 53rd AIAA Aerospace Sciences Meeting. 2015. doi: 10.2514/6.2015-1736
|
[7] |
王文, 蒋华兵. 钝锥表面脉动压力风洞试验研究[J]. 装备环境工程, 2021, 18(3): 45–50.
WANG W, JIANG H B. Wind tunnel test research on surface pressure fluctuations of a blunt cone[J]. Equipment Environmental Engineering, 2021, 18(3): 45–50.
|
[8] |
陈久芬, 凌岗, 张庆虎, 等. 7°尖锥高超声速边界层转捩红外测量实验[J]. 实验流体力学, 2020, 34(1): 60–66. doi: 10.11729/syltlx20180172
CHEN J F, LING G, ZHANG Q H, et al. Infrared thermography experiments of hypersonic boundary-layer transition on a 7°half-angle sharp cone[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(1): 60–66. doi: 10.11729/syltlx20180172
|
[9] |
易仕和, 刘小林, 牛海波, 等. 高超声速边界层流动稳定性实验研究[J]. 空气动力学学报, 2020, 38(1): 137–142.
YI S H, LIU X L, NIU H B, et al. Experimental study on flow stability of hypersonic boundary layer[J]. Acta Aero-dynamica Sinica, 2020, 38(1): 137–142.
|
[10] |
刘小林. 高超声速条件下圆锥边界层转捩相关实验研究[D]. 长沙: 国防科技大学, 2019.
LIU X L. Experimental investigation of the hypersonic boundary layer transition on the cones[D]. Changsha: National University of Defense Technology, 2019.
|
[11] |
JULIANO T, SCHNEIDER S. Instability and transition on the HIFiRE-5 in a Mach 6 quiet tunnel[C]//Proc of the 40th Fluid Dynamics Conference and Exhibit. 2010. doi: 10.2514/6.2010-5004
|
[12] |
WHEATON B M, BERRIDGE D C, WOLF T D, et al. Boundary layer transition (BOLT) flight experiment overview[C]//Proc of the 2018 Fluid Dynamics Conference. 2018. doi: 10.2514/6.2018-2892
|
[13] |
BERRIDGE D C, MCKIERNAN G, WADHAMS T P, et al. Hypersonic ground tests in support of the boundary layer transition (BOLT) flight experiment[C]//Proc of the 2018 Fluid Dynamics Conference. 2018. doi: 10.2514/6.2018-2893
|
[14] |
THOME J, DWIVEDI A, NICHOLS J W, et al. Direct numerical simulation of BOLT hypersonic flight vehicle[C]//Proc of the 2018 Fluid Dynamics Conference. 2018. doi: 10.2514/6.2018-2894
|
[15] |
MOYES A, KOCIAN T S, MULLEN C D, et al. Pre-flight boundary-layer stability analysis of BOLT geometry[C]//Proc of the 2018 Fluid Dynamics Conference. 2018. doi: 10.2514/6.2018-2895
|
[16] |
KOSTAK H, BOWERSOX R D, MCKIERNAN G, et al. Freestream disturbance effects on boundary layer instability and transition on the AFOSR BOLT geometry[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0088
|
[17] |
COOK D A, THOME J, NICHOLS J W, et al. Receptivity analysis of BOLT to distributed surface roughness using input-output analysis[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0089
|
[18] |
BERRIDGE D C, KOSTAK H, MCKIERNAN G, et al. Hypersonic ground tests with high-frequency instrumentation in support of the boundary layer transition (BOLT) flight experiment[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0090
|
[19] |
BERRY S A, MASON M L, GREENE F, et al. LaRC aerothermodynamic ground tests in support of BOLT flight experiment[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0091
|
[20] |
高清, 李建华, 李潜. 升力体高超声速飞行器横向气动特性研究[J]. 实验流体力学, 2015, 29(1): 43–48. doi: 10.11729/syltlx20130107
GAO Q, LI J H, LI Q. Study on lateral stability of hypersonic lifting-configurations[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(1): 43–48. doi: 10.11729/syltlx20130107
|
[21] |
LIU S S, YUAN X X, LIU Z Y, et al. Design and transition characteristics of a standard model for hypersonic boundary layer transition research[J]. Acta Mechanica Sinica, 2021, 37(11): 1637–1647. doi: 10.1007/s10409-021-01136-5
|
[22] |
陈坚强, 涂国华, 万兵兵, 等. HyTRV流场特征与边界层稳定性特征分析[J]. 航空学报, 2021, 42(6): 124317.
CHEN J Q, TU G H, WAN B B, et al. Characteristics of flow field and boundary-layer stability of HyTRV[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(6): 124317.
|
[23] |
陈曦, 董思卫, 袁先旭, 等. 升力体(HyTRV)边界层全局稳定性分析[C]//第十九届全国激波与激波管学术会议论文集. 2020.
|
[24] |
罗纪生. 高超声速边界层的转捩及预测[J]. 航空学报, 2015, 36(1): 357–372.
LUO J S. Transition and prediction for hypersonic boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 357–372.
|