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连云港港主体港区口门浅滩深水航道三维横流特性研究 被引量:2
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作者 熊伟 《人民珠江》 2017年第11期50-54,共5页
应用基于有限体积法的FVCOM建立了连云港海域的三维潮流数学模型,利用详细的实测水文资料进行了验证,结果较为满意。研究了连云港港主体港区旗台防波堤口门区域的三维潮流特征和浅滩深水航道的三维横流特性。结果表明,受北防波堤挑流影... 应用基于有限体积法的FVCOM建立了连云港海域的三维潮流数学模型,利用详细的实测水文资料进行了验证,结果较为满意。研究了连云港港主体港区旗台防波堤口门区域的三维潮流特征和浅滩深水航道的三维横流特性。结果表明,受北防波堤挑流影响,口门段航道最大横流出现在北防波堤堤头附近的航道横断面内,其中涨潮最大横流发生在中潮位前后1 h内,落潮最大横流发生在高潮位后1~2 h内。航道内表层和中层的横流数值较为接近,但由于航道内深层水流受航道约束更大,底层横流数值减小迅速。 展开更多
关键词 三维横流 浅滩深水航道 防波堤 FVCOM
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FURTHER OBSERVATIONS OF LATE TRANSITION PROCESSES IN CROSSFLOW INSTABILITY EXPERIMENT
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作者 吴永健 明晓 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2000年第1期26-30,共5页
The experiments of primary and secondary instabilities with controlled excitation are carried out on a swept flat plate to study the process leading to the final breakdown of laminar flow. Two types of high frequency ... The experiments of primary and secondary instabilities with controlled excitation are carried out on a swept flat plate to study the process leading to the final breakdown of laminar flow. Two types of high frequency secondary instabilities are identified. The most amplified mode is centered about the inflection point of the crosswise profile of the boundary layer and is interpreted as inflectional instability, the other occurs in the one third of the boundary layer from the wall. The high frequency disturbances are highly amplified but they also saturate similarly to the primary and nonlinearly generated disturbances. Their main effect in the final breakdown seems interact with the disturbances is developed and thus widens the frequency spectrum to turbulent state. 展开更多
关键词 three dimensional boundary layer cross flow instability secondary instability final onset of transition BREAKDOWN
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3-D NUMERICAL COMPUTATION OF JET ARRAY IMPINGEMENT WITH INITIAL CROSSFLOW 被引量:2
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作者 LIYong-kang ZHANGJing-zhou TANXiao-ming 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2004年第2期128-133,共6页
The 3-D numerical computation of the flow and temperature fields for jet array impingement with initial crossflow investigates the effects of the jet-to-surface spacing, the impinging hole arrangement and the jet-to-c... The 3-D numerical computation of the flow and temperature fields for jet array impingement with initial crossflow investigates the effects of the jet-to-surface spacing, the impinging hole arrangement and the jet-to-crossflow mass flux ratio on heat transfer characteristics. The study shows that: (1) under the different jet-to-surface spacing, the impingement cooling with inline arrangement is better than that with staggered arrangement for a given jet-to-crossflow mass flux ratio;( 2 ) the value of jet-to-surface spacing impacts a complicated effect on the flow and heat transfer for jet array impingement; (3) as the ratio of crossflow-to-jet mass flux ratio increases, the cooling effectiveness on monotonous decrease for both inline and staggered arrangements at the same jet-to-surface spacing. 展开更多
关键词 jet impingement numerical calculation enhanced heat transfer
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高超声速有攻角锥裙直接数值模拟
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作者 赖江 范召林 +3 位作者 王乾 董思卫 童福林 袁先旭 《航空学报》 EI CAS CSCD 北大核心 2024年第2期44-62,共19页
采用直接数值模拟方法对有攻角的高超声速7°~34°锥裙开展了数值研究,通过对比0°、90°、180°周向子午面,评估了三维横流效应对激波/边界层干扰的影响规律和作用机制,包括壁面压力、摩阻、热流分布,分离泡非定... 采用直接数值模拟方法对有攻角的高超声速7°~34°锥裙开展了数值研究,通过对比0°、90°、180°周向子午面,评估了三维横流效应对激波/边界层干扰的影响规律和作用机制,包括壁面压力、摩阻、热流分布,分离泡非定常运动,再附边界层演化等。研究发现,不同周向站位均出现流动分离,横流区、迎风区内复杂激波结构与边界层相互作用导致壁面压力、摩阻、热流显著升高。热流与压力的比值在干扰区上升后由于再附降低,而热流与摩阻的雷诺比拟关系在分离区则完全失效。分离泡面积脉动的功率谱结果表明,分离泡非定常膨胀/收缩运动呈低频特征,且分离泡呼吸与激波低频振荡在横流区密切相关,在迎风区存在迟滞,而在背风区不相关。速度脉动场的本征正交分解结果表明,分离区的低频特征与低阶模态相应的剪切层附近大尺度结构相关。对下游再附边界层演化分析指出,攻角的存在导致雷诺应力在再附点附近大幅增强,其流向分量的恢复最为迅速,雷诺应力分量的峰值位置在背风区沿流向持续外移,而在迎风区、横流区已迅速向内层恢复。此外,雷诺应力各向异性不变量分布进一步表明干扰下游的近壁区湍流各向异性峰值在背风区弱于迎风区。 展开更多
关键词 激波/边界层干扰 高超声速 分离泡 三维横流效应 直接数值模拟
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