The Fast Simulation of Highly Flexible Flight Dynamics
The Fast Simulation of Highly Flexible Flight Dynamics
批准号:
1944318
负责人:
金额:
$0.0万
依托单位:
依托单位国家:
英国
项目类别:
Studentship
财政年份:
2017
资助国家:
英国
项目状态:
已结题
起止时间:
2017 至 --
中文摘要
点击翻译按钮获取中文摘要
英文摘要
A combined formulation of the finite element method and computational fluid dynamics could be used to simulate the flight dynamics of highly flexible aircraft, but this would result in a very computationally expensive problem which may require many hours to solve even with high performance computing resources. The purpose of the proposed project is to reduce the computational cost of the analysis of combined flight dynamics and aeroelastics for highly flexible aircraft through the use of alternative, lower order methods. The project would initially involve investigation into the state of the art low order structural dynamics and fluid dynamics methods. Based on the outcome of the literature review, methods would be chosen to investigate, extend and implement within a computer code. The code will then be verified, most probably using data collected from a highly flexible model aircraft built by a team at the Institute of Aeronautical Technology in Brazil. It is likely that the code may become complex due to the need to be able to model a full model in comparison to a "toy" case. Once verified, the code will be compared to current methods. The code will also be used to investigate design and control problems. For example, the coupling of large elastic deformations between different parts of an aircraft or stability control methods for flexible aircraft. The motivation for this project is the need to increase aircraft efficiency. In order to do this, lighter airframes and higher aspect ratios must be used. In order for traditional flight dynamics laws to be used, the airframe must be stiff enough that the frequencies of the aeroelastics and the flight dynamics are dissimilar. By removing this stiffness constraint, more efficient aircraft may be designed at the cost of extensive consideration of the coupling between aeroelastics and flight dynamics. Analysing this is currently challenging, and is therefore a constraint the industry's ability to improve aircraft efficiency.
期刊论文(2)
专著(0)
科研奖励(0)
会议论文
Theoretical and computational studies of a rectangular finite wing oscillating in pitch and heave
矩形有限机翼俯仰和升沉振荡的理论与计算研究
DOI:
--
发表时间:
2018
期刊:
影响因子:
--
作者:
[Bird Hja]
通讯作者:
Bird Hja
DOI:
10.2514/6.2019-1377
发表时间:
2019
期刊:
影响因子:
--
作者:
[Bird H]
通讯作者:
Bird H
国内基金
海外基金
Simulation and certification of the ground state of many-body systems on quantum simulators
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批准号:--
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项目类别:--
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资助金额:40万元
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批准年份:2020
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负责人:Abolfazl Bayat
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依托单位: