Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory
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Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory
Vol. 27, Issue 7, (2012)
作者机构:
1. 中国空气动力研究与发展中心 空气动力学国家重点实验室,四川,绵阳,621000
2. 中国空气动力研究与发展中心 设备设计及测试技术研究所,四川,绵阳,621000
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Published:2012
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CONG Cheng-hua, PENG Qiang, WANG Fu-bo, et al. Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory[J]. 2012, 27(7).
DOI:
CONG Cheng-hua, PENG Qiang, WANG Fu-bo, et al. Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory[J]. 2012, 27(7).DOI:
Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory
Performance of icing wind tunnel's contraction section was investigated by numerical simulation.For several typical wall contours were provided by former researchers
the flow field calculation using simplified 2-D (two-dimensional)model was performed
and the pressures along the centerline and the velocity distribution at the test section entrance were obtained.The numerical simulation results show that all contraction curves can prevent the separation of boundary layers
and the difference of fluid dynamics parameters is negligible except for cubic curve and fifth power curve(xm=0.4) which can't provide a specified degree of uniformity.Then droplet trajectory was studied by numerical simulation when different diameter water-liquid that the droplets were released.The numerical results state droplet accretion using Witozinsky curve is less compared with that designed by other curves.By comparing of several contraction curves' effect on flow field and droplet trajectory
it can be concluded that convergent section designed by fifth power curve (xm=0.5) has higher efficiency.
Experimental and computational investigation into ice accretion on airfoil of a transport aircraft
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Comparison on flow field characteristics of four wind tunnel contraction sections
Experiment on airfoil runback ice protection based on synthetic jet,
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Related Institution
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