Collaborative Research: A fundamental study on supercooled large droplets: impacting, splashing, surface water dynamics, and ice accretion
合作研究:过冷大液滴的基础研究:撞击、飞溅、地表水动力学和积冰
基本信息
- 批准号:1916380
- 负责人:
- 金额:$ 28.12万
- 依托单位:
- 依托单位国家:美国
- 项目类别:Standard Grant
- 财政年份:2019
- 资助国家:美国
- 起止时间:2019-07-01 至 2024-06-30
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
Supercooled large droplets (SLDs), which include freezing drizzle drops and freezing raindrops, are up to 100 times larger than the cloud-sized droplets that are involved in most in-flight aircraft icing incidents. When SLDs impinge on airframe surfaces, they often impact on regions beyond the protection of current anti-/de-icing systems and splash into secondary droplets that sprinkle unprotected areas. This causes surface water runback and uncontrolled ice accretion. Aircraft icing due to SLDs, which occurs more frequently than first thought, is now recognized as a significant hazard. This collaborative research project will use a combination of experiments and modeling to understand underlying physics of SLD icing phenomena so that effective anti-/de-icing measures can be implemented to ensure safer and more efficient operation of aircraft in cold weather. The research team will collaborate scientists at other government agencies and aerospace companies to further broaden the impacts of the research. The project will train graduate and undergraduate students in research and will develop educational tools that will inspire high school students, especially those from groups underrepresented in STEM fields, to continue in science and engineering studies.The overall goal of this collaborative research is to conduct an integrated theoretical, numerical and experimental research to quantify important micro-physical processes, such as droplet impact, rebounding, splashing, surface water runback, and ice accretion, that are pertinent to SLD icing phenomena. Results will improve our understanding of the underlying physics for safer and more efficient operation of aircraft in atmospheric icing conditions. The research tasks include: 1) develop an SLD icing simulation tool based on a validated multiphase flow solver with a novel moment of fluid interface representation method; 2) conduct theoretical, experimental and numerical studies to characterize droplet impinging, rebounding and splashing on dry and wet surfaces pertinent to SLD icing to develop droplet impact models that contain a comprehensive consideration of controlling factors ignored in previous studies; and 3) perform an integrated numerical and experimental investigation to examine the characteristics of surface water runback and its effects on SLD icing. The research program will be incorporated into undergraduate and graduate curricula by adding a new teaching module and creating new courseware to stimulate students? interests in thermal-fluid sciences. Students from underrepresented groups will be recruited proactively to work on the proposed research to promote participation in science and engineering.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.
过冷大水滴 (SLD),包括冻毛毛雨和冻雨滴,比大多数飞行中飞机结冰事故中涉及的云大小水滴大 100 倍。 当 SLD 撞击机身表面时,它们通常会影响当前防冰/除冰系统保护范围之外的区域,并溅入二次液滴,洒落在未受保护的区域。 这会导致地表水回流和不受控制的积冰。 由于 SLD 导致的飞机结冰发生的频率比最初想象的要高,现在被认为是一种重大危险。该合作研究项目将结合实验和建模来了解SLD结冰现象的基本物理原理,以便实施有效的防/除冰措施,确保飞机在寒冷天气下更安全、更高效地运行。 研究小组将与其他政府机构和航空航天公司的科学家合作,进一步扩大研究的影响。 该项目将培训研究生和本科生进行研究,并将开发教育工具,激励高中生,特别是那些来自 STEM 领域代表性不足的群体的学生,继续进行科学和工程研究。这项合作研究的总体目标是进行综合理论、数值和实验研究,以量化重要的微观物理过程,例如水滴撞击、反弹、飞溅、地表水回流和冰积聚,这些过程 与 SLD 结冰现象有关。 研究结果将提高我们对基础物理的理解,使飞机在大气结冰条件下更安全、更高效地运行。研究任务包括:1)开发基于经过验证的多相流求解器和新颖的流体界面矩表示方法的SLD结冰模拟工具; 2)进行理论、实验和数值研究,以表征与SLD结冰相关的干湿表面上的液滴撞击、反弹和飞溅特征,以开发液滴撞击模型,该模型全面考虑了先前研究中忽略的控制因素; 3) 进行综合数值和实验研究,以检验地表水回流的特征及其对 SLD 结冰的影响。 该研究计划将通过添加新的教学模块和创建新的课件来融入本科生和研究生课程中以激发学生的兴趣?对热流体科学感兴趣。 来自代表性不足群体的学生将被积极招募来从事拟议的研究,以促进对科学和工程的参与。该奖项反映了 NSF 的法定使命,并通过使用基金会的智力价值和更广泛的影响审查标准进行评估,被认为值得支持。
项目成果
期刊论文数量(9)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
A field study of ice accretion and its effects on the power production of utility-scale wind turbines
- DOI:10.1016/j.renene.2020.12.014
- 发表时间:2021-01-15
- 期刊:
- 影响因子:8.7
- 作者:Gao, Linyue;Tao, Tao;Hu, Hui
- 通讯作者:Hu, Hui
An experimental study to characterize the effects of initial ice roughness on the wind-driven water runback over an airfoil surface
- DOI:10.1016/j.ijmultiphaseflow.2020.103254
- 发表时间:2020-05
- 期刊:
- 影响因子:3.8
- 作者:Yang Liu;Kai Zhang;W. Tian;Hui Hu
- 通讯作者:Yang Liu;Kai Zhang;W. Tian;Hui Hu
Experimental Study of Dynamic Ice Accretion Process over Rotating Aeroengine Fan Blades
- DOI:10.2514/1.t6667
- 发表时间:2022-11
- 期刊:
- 影响因子:2.1
- 作者:L. Tian;Linkai Li;Haiyang Hu;Hui Hu
- 通讯作者:L. Tian;Linkai Li;Haiyang Hu;Hui Hu
An Experimental Study on Mitigating Dynamic Ice Accretion Process on Bridge Cables with a Superhydrophobic Coating
- DOI:10.1016/j.expthermflusci.2021.110573
- 发表时间:2021-12
- 期刊:
- 影响因子:3.2
- 作者:Yihua Peng;R. Veerakumar;Zichen Zhang;Haiyang Hu;Yang Liu;Xuhui He;Hui Hu
- 通讯作者:Yihua Peng;R. Veerakumar;Zichen Zhang;Haiyang Hu;Yang Liu;Xuhui He;Hui Hu
An experimental study on the transient runback characteristics of wind-driven film/rivulet flows
- DOI:10.1063/5.0067672
- 发表时间:2021-11
- 期刊:
- 影响因子:4.6
- 作者:Kai Zhang;Hui Hu
- 通讯作者:Kai Zhang;Hui Hu
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Hui Hu其他文献
Constrained solution of CEC 2017 with monarch butterfly optimisation
CEC 2017 帝王蝶优化的约束解
- DOI:
10.1504/ijwmc.2019.10020382 - 发表时间:
2019-04 - 期刊:
- 影响因子:0
- 作者:
Song Hu;Hui Hu;Jia Chen;Yingxue Cai;Sibo Huang;Zhaoquan Cai - 通讯作者:
Zhaoquan Cai
Safety Assessment of Road Passenger Transportation Enterprise on Key Criteria
道路客运企业关键指标安全评价
- DOI:
10.4156/aiss.vol5.issue9.3 - 发表时间:
2013-05 - 期刊:
- 影响因子:0
- 作者:
Hui Hu;Jingshuai Yang;Liangmin Li;Dawei Hu - 通讯作者:
Dawei Hu
On approximate solutions of infinite systems of linear inequalities
关于无限线性不等式系统的近似解
- DOI:
- 发表时间:
1989 - 期刊:
- 影响因子:0
- 作者:
Hui Hu;Qing Wang - 通讯作者:
Qing Wang
Investigation on Mechanical Properties of S30403 Austenitic Stainless Steel at Different Temperatures
S30403奥氏体不锈钢不同温度力学性能研究
- DOI:
10.1115/1.4039123 - 发表时间:
2018-01 - 期刊:
- 影响因子:1
- 作者:
Lu Yaqing;Hui Hu - 通讯作者:
Hui Hu
Three Mn(II) complexes based on 6-(3-pyridyl)isophthalic acid ligand:
三种基于 6-(3-吡啶基)间苯二甲酸配体的 Mn(II) 配合物:
- DOI:
- 发表时间:
2017 - 期刊:
- 影响因子:2.6
- 作者:
Xiuling Zhang;Na Wang;Peng-Fei Liu;Da-Shuai Zhang;Hui Hu - 通讯作者:
Hui Hu
Hui Hu的其他文献
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{{ truncateString('Hui Hu', 18)}}的其他基金
A Fundamental Study on Unsteady Heat Transfer and Dynamic Ice Accretion Processes Pertinent to UAV Icing Protection
与无人机防冰相关的非稳态传热和动态积冰过程的基础研究
- 批准号:
2313310 - 财政年份:2023
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
PFI-TT: Development of A New Class of Low-Power, Plasma-Based Wind Turbine Icing Protection Systems
PFI-TT:开发新型低功率等离子体风力涡轮机结冰保护系统
- 批准号:
2140489 - 财政年份:2022
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
A Fundamental Study Toward Innovative Plasma-Based Anti-/De-icing Strategies for Aircraft Icing Mitigation
针对飞机结冰的创新型等离子体防/除冰策略的基础研究
- 批准号:
1935363 - 财政年份:2020
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
NNA: Bridging the Atomistic Deformation Mechanisms to the Microscopic Adhesive-to-Cohesive Fracture at Ice-Metal Interfaces
NNA:将原子变形机制与冰-金属界面处的微观粘着-内聚断裂联系起来
- 批准号:
1824840 - 财政年份:2018
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
Quantification of Wind-Driven Surface Water Transport Process for Aircraft Icing Studies
飞机结冰研究中风力驱动的地表水输送过程的量化
- 批准号:
1435590 - 财政年份:2014
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
Innovative Dual-Rotor Wind Turbine (DRWT) Designs for Improved Turbine Performance and Wind Farm Efficiency
创新的双转子风力涡轮机 (DRWT) 设计可提高涡轮机性能和风电场效率
- 批准号:
1438099 - 财政年份:2014
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
Characterization of Surface Wind Energy Resources and Wake Interferences among Wind Turbines over Complex Terrains for Optimal Site Design and Turbine Durability
复杂地形上地面风能资源和风力涡轮机尾流干扰的表征,以实现最佳场地设计和涡轮机耐久性
- 批准号:
1133751 - 财政年份:2012
- 资助金额:
$ 28.12万 - 项目类别:
Continuing Grant
Icing Physics Studies Pertinent to Wind Turbine Icing and De/Anti-icing
与风力涡轮机结冰和除冰/防冰相关的结冰物理研究
- 批准号:
1064196 - 财政年份:2011
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
IRES: US-China Collaboration on Bio-Inspired Aerodynamic Designs for the Development of Next Generation Micro Air Vehicles
IRES:美中合作开发下一代微型飞行器的仿生空气动力学设计
- 批准号:
1064235 - 财政年份:2011
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
CAREER: Development of a Molecule-based Diagnostic Technique to Study Joule Heating and Micro-scale Heat Transfer Process in Electrokinetically-driven Microfluidics
职业:开发基于分子的诊断技术来研究电动驱动微流体中的焦耳热和微尺度传热过程
- 批准号:
0545918 - 财政年份:2006
- 资助金额:
$ 28.12万 - 项目类别:
Standard Grant
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