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飞翼布局飞机耦合运动失稳的主动流动控制 被引量:9
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作者 冯立好 魏凌云 +1 位作者 董磊 王晋军 《航空学报》 EI CAS CSCD 北大核心 2022年第10期137-148,共12页
飞翼布局飞机是现代先进飞行器设计的重要构型之一。由于缺乏平尾、垂尾等传统舵面,飞翼布局飞机在大攻角状态面临滚转、滚转与俯仰耦合、滚转与偏航耦合等失稳问题,严重影响飞机气动性能及飞行安全。对此开展了合成射流主动控制研究,... 飞翼布局飞机是现代先进飞行器设计的重要构型之一。由于缺乏平尾、垂尾等传统舵面,飞翼布局飞机在大攻角状态面临滚转、滚转与俯仰耦合、滚转与偏航耦合等失稳问题,严重影响飞机气动性能及飞行安全。对此开展了合成射流主动控制研究,提出了通过增强前缘涡进而改善动态稳定性的控制策略,分析了合成射流对飞翼布局滚转及其耦合运动的控制规律,揭示了飞翼布局飞机动态运动及耦合效应对合成射流控制效果的影响机理。研究结果表明,布置于飞翼布局飞机机翼前缘的合成射流可以有效增强前缘涡,进而改变气动力及力矩,特别是采用与滚转运动角速度方向相反的控制力矩策略能够增加滚转阻尼,改善横向稳定性。本文结果可为飞翼布局飞机增稳控制提供重要的技术支撑。 展开更多
关键词 飞翼布局飞机 耦合运动 失稳 合成射流 动态控制
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格尼襟翼对旋转导弹气动特性的影响
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作者 寇少博 冯立好 +3 位作者 李晓 杨欣 刘松彬 徐华松 《空气动力学学报》 CSCD 北大核心 2023年第1期77-85,共9页
旋转导弹多采用斜置尾翼产生滚转力矩,但存在转速稳定性差等问题,影响了命中精度。为改善旋转导弹气动特性,本文采用在导弹尾翼后缘放置格尼襟翼的方式代替传统斜置尾翼产生滚转力矩。通过数值模拟方法,研究了不同高度格尼襟翼对导弹气... 旋转导弹多采用斜置尾翼产生滚转力矩,但存在转速稳定性差等问题,影响了命中精度。为改善旋转导弹气动特性,本文采用在导弹尾翼后缘放置格尼襟翼的方式代替传统斜置尾翼产生滚转力矩。通过数值模拟方法,研究了不同高度格尼襟翼对导弹气动特性的影响规律,并与斜置尾翼模型进行对比。结果表明:格尼襟翼能够产生保持导弹旋转的滚转力矩,且格尼襟翼高度增加,滚转力矩增大;相比斜置尾翼,格尼襟翼能够为导弹提供更大的滚转力矩,对导弹侧向力的影响相对更小。不同来流马赫数下格尼襟翼的操纵效率略有差异,亚声速来流时,格尼襟翼产生的滚转力矩随着导弹迎角增加而减小;超声速来流时,格尼襟翼产生的滚转力矩几乎不随迎角变化而改变,与亚声速来流相比,格尼襟翼的操纵效率降低。进一步通过分析流场揭示了格尼襟翼产生滚转力矩的流动机理:格尼襟翼使得导弹尾翼后缘附近产生非对称流动,以致各尾翼出现非对称的压力差,从而产生保持导弹旋转的滚转力矩。 展开更多
关键词 旋转导弹 格尼襟翼 气动特性 滚转力矩
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Enhancing Geological Understanding and Identifying Gold Anomalies in the Ailaoshan Orogen
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作者 ZHAO Shiyu YANG Lin +5 位作者 SONG Yiwei DONG Yuntao feng lihao LI Huajian WU Junyu WANG Qingfei 《Acta Geologica Sinica(English Edition)》 SCIE CAS CSCD 2024年第2期441-453,共13页
The Ailaoshan Orogen in the southeastern Tibet Plateau,situated between the Yangtze and Simao blocks,underwent a complex structural,magmatic,and metamorphic evolution resulting in different tectonic subzones with vary... The Ailaoshan Orogen in the southeastern Tibet Plateau,situated between the Yangtze and Simao blocks,underwent a complex structural,magmatic,and metamorphic evolution resulting in different tectonic subzones with varying structural lineaments and elemental concentrations.These elements can conceal or reduce anomalies due to the mutual effect between different anomaly areas.Dividing the whole zone into subzones based on tectonic settings,ore cluster areas,or sample catchment basins(Scb),geochemical and structural anomalies associated with gold(Au)mineralization have been identified utilizing mean plus twice standard deviations(Mean+2STD),factor analysis(FA),concentration-area(CA)modeling of stream sediment geochemical data,and lineament density in both the Ailaoshan Orogen and the individual subzones.The FA in the divided 98 Scbs with 6 Scbs containing Au deposits can roughly ascertain unknown rock types,identify specific element associations of known rocks and discern the porphyry or skarn-type Au mineralization.Compared with methods of Mean+2STD and C-A model of data in the whole orogen,which mistake the anomalies as background or act the background as anomalies,the combined methods of FA and C-A in the separate subzones or Scbs works well in regional metallogenic potential analysis.Mapping of lineament densities with a 10-km circle diameter is not suitable to locate Au deposits because of the delineated large areas of medium-high lineament density.In contrast,the use of circle diameters of 1.3 km or 1.7 km in the ore cluster scale delineates areas with a higher concentration of lineament density,consistent with the locations of known Au deposits.By analyzing the map of faults and Au anomalies,two potential prospecting targets,Scbs 1 and 63 with a sandstone as a potential host rock for Au,have been identified in the Ailaoshan Orogen.The use of combined methods in the divided subzones proved to be more effective in improving geological understanding and identifying mineralization anomalies associated with Au,rather than analyzing the entire large area. 展开更多
关键词 minerology GEOCHEMISTRY GOLD stream sediment sample catchment basin concentration-area model lineament density Ailaoshan Orogen
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基于吹吸气控制的飞行器大攻角气动性能提升方法研究
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作者 李晓 刘晓冬 +4 位作者 冯立好 李璞 肖伶 石钧之 衣然 《力学学报》 2026年第1期1-14,共14页
流动控制是改善飞行器气动性能,拓展飞行包线的重要途径.以往流动控制设计较少考虑实际流动情况,导致控制方法和参数设计存在难实现等问题.本文提出了通过吹吸气调控前缘涡进而改善大攻角气动性能的涡扰动控制原理,以一个飞翼布局飞机为... 流动控制是改善飞行器气动性能,拓展飞行包线的重要途径.以往流动控制设计较少考虑实际流动情况,导致控制方法和参数设计存在难实现等问题.本文提出了通过吹吸气调控前缘涡进而改善大攻角气动性能的涡扰动控制原理,以一个飞翼布局飞机为例,阐述了如何依据未控制工况的翼面流动压力信息设计控制参数,并且验证了控制效果和可操作性.首先,研究了一个后掠角为65°的小展弦比飞翼标模的纵向气动特性,发现该飞翼标模会在38°攻角下发生升力失速和力矩失速.其次,在涡扰动控制原理的指导下,设计了沿飞行器前缘分布的4个吹吸气狭缝,研究了在机翼不同位置分别施加吹气、吸气时的控制效果.进一步,设计了前段狭缝吹气与后段狭缝吸气联合控制方法,翼面压强分布和控制参数设计表明,该方法可将吸气口吸入的气体经由吹气口吹出,从而可在不依赖外部气源供气的情况下实现控制.控制效果分析表明,吹吸气联合控制能够增强前缘涡强度和负压,延缓前缘涡破裂,进而显著提高后失速阶段的升力系数,延缓失速后升力系数和俯仰力矩系数的掉落,拓展飞行包线.综上,本文提出的控制原理和方法基于飞行器翼面实际流动情况设计,方法有效、可操作性强,具有重要价值. 展开更多
关键词 飞翼布局 前缘涡 涡扰动控制原理 吹吸气联合控制
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Review of zero-net-mass-flux jet and its application in separation flow control 被引量:30
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作者 ZHANG Panfeng WANG JinJun feng lihao 《Science China(Technological Sciences)》 SCIE EI CAS 2008年第9期1315-1344,共30页
Since the zero-net-mass-flux (ZNMF) jet was first used as a laboratory flow control method in 1990's, it has attracted much attention. The ZNMF jet has unique features such as compact actuator, no requirement for ... Since the zero-net-mass-flux (ZNMF) jet was first used as a laboratory flow control method in 1990's, it has attracted much attention. The ZNMF jet has unique features such as compact actuator, no requirement for external air supply, complex piping, etc., and becomes a hot topic research subject in fluid mechanics. This review introduces the state of the art in the development of ZNMF jet in the quiescent fluid, the interaction of the ZNMF jet with the cross flow and its application in the separation flow control. The evolution of the vortex ring/pair and the spacial flow structure of the ZNMF in quicent fluid or cross flow are presented, as well as the key parameter effects. At last, the applications of ZNMF jet in the wake control of the circular cylinder, the separation control on the airfoil and the aerodynamic force or moment control on MAV/UAV are presented. 展开更多
关键词 zero-net-mass-flux JET quiescent fluid cross flow SEPARATION control
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Experimental investigation on control of vortex shedding mode of a circular cylinder using synthetic jets placed at stagnation points 被引量:12
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作者 MA LiQun feng lihao 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第1期158-170,共13页
Control of flow around a circular cylinder by synthetic jets has been experimentally investigated in a water tunnel with particle image velocimetry(PIV) technique.The synthetic jets are positioned at both the front an... Control of flow around a circular cylinder by synthetic jets has been experimentally investigated in a water tunnel with particle image velocimetry(PIV) technique.The synthetic jets are positioned at both the front and rear stagnation points.With power spectrum analysis,proper orthogonal decomposition(POD) method and other techniques for data processing,particular attention is paid to the control of vortical structures around the circular cylinder,in which the excitation frequency f e is one to three times of the natural frequency f0 and the cylinder Reynolds number and the excitation amplitude are fixed.The influenced-scope of the synthetic jet enlarges as the excitation frequency increases,and thus the synthetic jet dominates the global flow field gradually.For the natural case and the control case at fe/f0=1,the distributions of the first two POD modes and the power spectra for their POD coefficients all exhibit the characteristics of the natural shedding with antisymmetric mode.For fe/f0=2 and fe/f0=3,the variations in the third and fourth POD modes and the corresponding power spectra indicate that the wake vortex shedding mode changes and the dominant frequency becomes the excitation frequency.For fe/f0=2,the wake vortex sheds downstream with either the antisymmetric or the symmetric mode;for fe/f0=3,the synthetic jet vortex pair interacts with the near wake shear layers from both sides to induce a pair of the symmetric wake vortices,which is gradually converted into an antisymmetric mode when shedding downstream. 展开更多
关键词 flow control synthetic jet circular cylinder stagnation points wake vortex shedding mode
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Fourier mode decomposition of PIV data. 被引量:8
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作者 MA LiQun feng lihao +2 位作者 PAN Chong GAO Qi WANG JinJun 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2015年第11期1935-1948,共14页
The modal decomposition technique is one of the most effective methods for studying the flow dynamics in a complex flow. By rejuvenating the discrete Fourier transform(DFT), this paper proposes a Fourier mode decompos... The modal decomposition technique is one of the most effective methods for studying the flow dynamics in a complex flow. By rejuvenating the discrete Fourier transform(DFT), this paper proposes a Fourier mode decomposition(FMD) method for the time series of particle image velocimetry(PIV) data from the fluid field. An experimental case concerning the control of the flow around a circular cylinder by a synthetic jet positioned at the rear stagnation point is used to demonstrate the use of the FMD method. In the three different regimes where the natural shedding frequency and actuation frequency dominate respectively or simultaneously, it is found that the FMD method is capable of extracting the dynamic mode along with its amplitude and phase according to the selected characteristic frequency based on the global power spectrum. For the quasiperiodic flow phenomena presented in this particular case, the FMD method can reconstruct the original flow field using the zero-th mode and the selected mode corresponding to the characteristic frequency. Similarities and differences between the FMD method and the dynamical mode decomposition(DMD) and proper orthogonal decomposition(POD) methods are also discussed. 展开更多
关键词 flow control vortex dynamics Fourier mode decomposition (FMD)
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Influence of orifice-to-wall distance on synthetic jet vortex ring simpinging on a fixed wall 被引量:3
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作者 XU Yang feng lihao 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第7期1798-1806,共9页
Two-dimensional particle image velocimetry (PIV) is used to investigate the influence of the orifice-to-wall distance on synthetic jet vortex rings impinging on a fixed wall. Both evolutions of vortical structures and... Two-dimensional particle image velocimetry (PIV) is used to investigate the influence of the orifice-to-wall distance on synthetic jet vortex rings impinging on a fixed wall. Both evolutions of vortical structures and statistical characteristics of flow fields at different orifice-to-wall distances are presented. It is found that different orifice-to-wall distances have different effects in terms of the vortex strength and impinging speed when the vortex rings are approaching the wall. The secondary vortex ring can be observed within the shear layer only when the dimensionless orifice-to-wall distance is close to or less than the dimensionless stroke length. Consequently, an appropriate orifice-to-wall distance plays a vital role in the sense of impingement effect. The statistical analysis of the flow field indicates that a wall jet forms after impingement, while both the decay rate of the maximum radial velocity and the spreading rate of the half-width decrease with the increasing orifice-to-wall distance. The non-dimensional wall jet velocity profiles at different orifice-to-wall distances all exhibit self-similar behaviors, which is consistent with the theoretical solution of the laminar wall jet. 展开更多
关键词 VORTEX ring orifice-to-wall DISTANCE IMPINGEMENT WALL secondary VORTEX statistical characteristic
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