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反铁磁质中超声波与自旋波的耦合模式
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作者 章惠康 《中南民族大学学报(自然科学版)》 CAS 2003年第S1期1-3,共3页
 计算和讨论了在反铁磁质中沿垂直外磁场方向传播的横超声波和自旋波的耦合模式的色散关系,此时磁声相互作用能与外磁场大小成正比,此耦合模式的色散关系与在铁磁质中沿平行的外磁场方向传播的磁声耦合模式的色散关系相似.
关键词 垂直的外磁场 反铁磁质 横超声波 耦合模式
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Self-recovery ability of stress-damaged salt rock experiment 被引量:1
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作者 De-yi JIANG Qiao-xian LI +2 位作者 Jie CHEN Song REN Chun-he YANG 《Journal of Coal Science & Engineering(China)》 2013年第1期63-68,共6页
After being compressed to different plastic deformation stages, the salt rock samples with lateral stress damage of 0.2, 0.3, 0.4, and 0.5 were selected. Ultrasonic technology was used to monitor the wave velocity var... After being compressed to different plastic deformation stages, the salt rock samples with lateral stress damage of 0.2, 0.3, 0.4, and 0.5 were selected. Ultrasonic technology was used to monitor the wave velocity variation law of stress-dam-aged salt rock during the self-recovery experiment under different temperatures to analyze the influence of initial stress damage and temperature during the self-recovery of salt rock. The experiment shows that the change of salt rock axial wave velocity is smaller than that of lateral wave velocity. The sample ultrasonic velocity is positively correlated with the time of self-recovery, and the damage had been recovered to a certain extent. In the first 200 hours of self-recovery stage, the salt rock lateral damage recovers fast, and then the damage remains almost unchanged. The value of lateral stable damage is positively correlated with the value of lateral initial stress damage. With the increase of temperature, the recovery of lateral damage speeds up and the value of stable damage decreases; the axial damage of salt rock almost remains unchanged during the self-recovery experiment. 展开更多
关键词 salt rock DAMAGE SELF-RECOVERY ULTRASONIC
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Effects of the injector geometry on a sonic jet into a supersonic crossflow 被引量:3
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作者 WANG GuoLei CHEN LiWei LU XiYun 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2013年第2期366-377,共12页
Large-eddy simulation of a sonic injection from circular and elliptic injectors into a supersonic crossflow has been performed.The effects of injector geometry on various fundamental mechanisms dictating the intricate... Large-eddy simulation of a sonic injection from circular and elliptic injectors into a supersonic crossflow has been performed.The effects of injector geometry on various fundamental mechanisms dictating the intricate flow phenomena including shock/jet interaction,jet shear layer vortices and their evolution,jet penetration properties and the relevant turbulence behaviors have been studied systematically.As a jet issuing transversely into a supersonic crossflow,salient three-dimensional shock and vortical structures,such as bow,separation and barrel shocks,Mach disk,horseshoe vortex,jet shear layer vortices and vortex pairs,are induced.The shock structures exhibit considerable deformations in the circular injection,while their fluctuation becomes smaller in the elliptic injection.The jet shear layer vortices are generated at the jet periphery and their evolution characteristics are analyzed through tracing the centroid of these coherent structures.It is found that the jet from the elliptic injector spreads rapidly in the spanwise direction but suffers a reduction in the transverse penetration compared to the circular injection case.The turbulent fluctuations are amplified because of the jet/crossflow interaction.The vertical Reynolds normal stress is enhanced in the downstream of the jet because of the upwash velocity induced by the counter-rotating vortex pair. 展开更多
关键词 large-eddy simulation compressible turbulence supersonic flow JET shock wave shock and turbulence interaction
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