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Response of a hypersonic blunt cone boundary layer to slow acoustic waves with assessment of various routes of receptivity 被引量:5
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作者 bingbing wan Jisheng LUO Caihong SU 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2018年第11期1643-1660,共18页
The hypersonic boundary-layer receptivity to slow acoustic waves is investigated for the Mach 6 flow over a 5-degree half-angle blunt cone with the nose radius of 5.08 mm. The plane acoustic wave interacts with the bo... The hypersonic boundary-layer receptivity to slow acoustic waves is investigated for the Mach 6 flow over a 5-degree half-angle blunt cone with the nose radius of 5.08 mm. The plane acoustic wave interacts with the bow shock, and generates all types of disturbances behind the shock, which may take various routes to generate the boundarylayer unstable mode. In this paper, two routes of receptivity are investigated in detail.One is through the disturbance in the entropy layer. The other is through the slow acoustic wave transmitted downstream the bow shock, which can excite the boundary-layer mode due to the synchronization mechanism. The results show that, for a low frequency slow acoustic wave, the latter route plays a leading role. The entropy-layer instability wave is able to excite the first mode near the neutral point, but its receptivity efficiency is much lower. 展开更多
关键词 RECEPTIVITY entropy layer blunt cone hypersonic boundary layer
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钝度对钝锥/楔熵层稳定性的影响研究
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作者 万兵兵 陈坚强 +3 位作者 涂国华 向星皓 袁先旭 段茂昌 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2023年第1期139-147,共9页
本文利用稳定性理论和数值模拟方法研究头部钝度对高超声速钝锥与钝楔的熵层稳定性的影响.结果表明钝楔的熵层不稳定性相比钝锥更强.随着钝度增加,熵层厚度逐渐变厚,熵层模态的不稳定性频率逐渐减小,但其不稳定区间不断向下游拓宽,表明... 本文利用稳定性理论和数值模拟方法研究头部钝度对高超声速钝锥与钝楔的熵层稳定性的影响.结果表明钝楔的熵层不稳定性相比钝锥更强.随着钝度增加,熵层厚度逐渐变厚,熵层模态的不稳定性频率逐渐减小,但其不稳定区间不断向下游拓宽,表明熵层中的扰动将有更多机会影响边界层的转捩过程.数值模拟实现了熵层模态激发边界层第一模态的过程. 展开更多
关键词 稳定性理论 稳定区间 边界层 不稳定性 钝锥 熵层 高超声速 数值模拟方法
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Effects of trace ytterbium addition on microstructure,mechanical and thermal properties of hypoeutectic Al-5Ni alloy 被引量:3
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作者 Kang wang Shaodong Hu +6 位作者 Yanglin Zhong Shuoxun Jin Zirong Zhou Zhiyu wang Jiongcai Chen bingbing wan Wenfang Li 《Journal of Rare Earths》 SCIE EI CAS CSCD 2022年第8期1305-1315,共11页
Over the past decade,the cast aluminum alloys with excellent mechanical and conductivity properties have emerged as potential materials for thermal management.However,the traditional Al-Si based alloys are difficult t... Over the past decade,the cast aluminum alloys with excellent mechanical and conductivity properties have emerged as potential materials for thermal management.However,the traditional Al-Si based alloys are difficult to make significant breakthrough in conductivity performance.The hypoeutectic Al-5Ni alloy also possesses sound castability and is expected to be applied in thermal management applications.In this study,the effects of ytterbium(Yb element) at 0-0.5 wt% on the microstructures as well as the electrical/thermal conductivity and mechanical properties of the Al-5Ni alloy were systematically investigated.The experimental results indicate that the addition of Yb at a relatively low amount not only reduces the secondary dendrite arm spacing of the α-Al grains,but also modifies the morphology and distribution of eutectic boundary phase.Moreover,it is found that the dosage of Yb at 0.3 wt% in the Al-5Ni alloy can simultaneously improve the yield strength,ultimate tensile strength and electrical/thermal conductivity.The strengthening and toughening of the Al-5Ni alloy are mainly attributed to the decrease of secondary dendrite arm spacing and the improvement of eutectic phases.The transmission electron microscopy/selected area electron diffraction(TEM/SAED) analysis indicates that the ytterbium in Al-5Ni alloy will form Al_(3)Yb phase,which mainly agglomerates in the Al_(3)Ni phase region.This phase is helpful to decrease the solubility of impurity elements(e.g.,Fe and Si) in the α-Al matrix,which is beneficial to electrical/thermal conductivity.The value of this study lays foundation for manufacturing Al-Ni alloys with high thermal conductivity and acceptable mechanical properties. 展开更多
关键词 Aluminum alloys Ytterbrium Trace dosage Mechanical properties Thermal conductivity Rare earths
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Progress in flight tests of hypersonic boundary layer transition 被引量:2
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作者 Guohua Tu Jianqiang Chen +7 位作者 Xianxu Yuan Qingtao Yang Maochang Duan Qiang Yang Yi Duan Xi Chen bingbing wan Xinghao Xiang 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2021年第11期1589-1609,I0001,共22页
Boundary layer transition(BLT)can cause a sharp rise in heat flux and skin friction,which can seriously affect the flight performance and safety of hypersonic flight vehicles.Therefore,the mechanism,prediction and con... Boundary layer transition(BLT)can cause a sharp rise in heat flux and skin friction,which can seriously affect the flight performance and safety of hypersonic flight vehicles.Therefore,the mechanism,prediction and control of transition have become important issues that must be dealt with for the development of advanced flight vehicles,and it is also a research hotspot of particular interest to major aerospace countries.Compared to other transition research approaches,model flight tests can better present the transition problems under real flight conditions,thus have been carried out extensively over the past 30 years.The United States,Germany,France,Australia,and other countries have carried out transition research based on flight tests,such as the Pegasus wing-glove crossflow transition and the Hypersonic Boundary Layer Transition(HyBOLT)transition control flight test of the United States,the joint research project of the Hypersonic International Flight Research and Experimentation-1(HIFiRE-1)circular cone and the HIFiRE-5 elliptic cone transition flight tests between the United States and Australia,the flight test of compression surface transition of the scramjet forebody(LEA)in France and so on.Although these flight tests suffered various setbacks,they still obtained valuable transition data.Recently,the United States is carrying out the concave-surface transition flight tests of Hypersonic Boundary Layer Transition(BOLT)and BOLT-II.Since its first model flight test mission for verification purpose launched successfully in 2015,several hypersonic BLT flight tests have been conducted by China Aerodynamics Research and Development Center(CARDC).The flight tests have measured valid transition data under flight conditions,obtained the transition front and its dynamical variation on blunt cones at various angles of attack and a lifting body Hypersonic Transition Research Vehicle(HyTRV).The crossflow traveling waves in high-altitude flight were measured for the first time,and our understanding of hypersonic BLT has been greatly improved. 展开更多
关键词 Hypersonic flow Boundary layer transition Flight test MF-1 HyTRV
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