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Stereo particle image velocimetry measurement of 3D soil deformation around laterally loaded pile in sand 被引量:6
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作者 袁炳祥 谌文武 +2 位作者 姜彤 汪亦显 陈科平 《Journal of Central South University》 SCIE EI CAS 2013年第3期791-798,共8页
A developed stereo particle image velocimetry(stereo-PIV) system was proposed to measure three-dimensional(3D) soil deformation around a laterally loaded pile in sand.The stereo-PIV technique extended 2D measurement t... A developed stereo particle image velocimetry(stereo-PIV) system was proposed to measure three-dimensional(3D) soil deformation around a laterally loaded pile in sand.The stereo-PIV technique extended 2D measurement to 3D based on a binocular vision model,where two cameras with a well geometrical setting were utilized to image the same object simultaneously.This system utilized two open software packages and some simple programs in MATLAB,which can easily be adjusted to meet user needs at a low cost.The failure planes form an angle with the horizontal line,which are measured at 27°-29°,approximately three-fourths of the frictional angle of soil.The edge of the strain wedge formed in front of the pile is an arc,which is slightly different from the straight line reported in the literature.The active and passive influence zones are about twice and six times of the diameter of the pile,respectively.The test demonstrates the good performance and feasibility of this stereo-PIV system for more advanced geotechnical testing. 展开更多
关键词 particle image velocimetry digital image correlation stereo particle image velocimetry laterally loaded pile scaledmodel 3D soil deformation soil-structural interaction
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机翼静气弹特性高速风洞试验研究
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作者 杨波 江翔 +1 位作者 马经忠 王国良 《气动研究与试验》 2024年第4期82-86,共5页
在连续式跨声速风洞中对某大展弦比机翼的静气动弹性特性进行了试验研究。试验结果表明,静气动弹性对机翼气动特性有明显影响,可使机翼零迎角升力系数和升力线斜率降低;在不同马赫数下,静气动弹性对机翼焦点位置的影响表现出不同规律,... 在连续式跨声速风洞中对某大展弦比机翼的静气动弹性特性进行了试验研究。试验结果表明,静气动弹性对机翼气动特性有明显影响,可使机翼零迎角升力系数和升力线斜率降低;在不同马赫数下,静气动弹性对机翼焦点位置的影响表现出不同规律,在低亚声速时使机翼焦点位置后移,超过一定马赫数后,弹性影响使机翼焦点位置前移;设计巡航点的副翼效率降低约34%,弹性变形后的机翼剖面扭转角分布与设计目标值较为接近,验证了机翼型架外形设计的合理性。 展开更多
关键词 静气动弹性 弹性相似模型 大展弦比 副翼效率
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