2013 Fiscal Year Final Research Report
Development of Preliminary Design Oriented CFD Solver and its Application to Environment Friendly Aircraft Design
| Project/Area Number |
23760767
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| Research Category |
Grant-in-Aid for Young Scientists (B)
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| Allocation Type | Multi-year Fund |
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| Research Field |
Aerospace engineering
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| Research Institution | The University of Tokyo |
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Principal Investigator |
IMAMURA Taro 東京大学, 工学(系)研究科(研究院), 准教授 (30371115)
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| Project Period (FY) |
2011 – 2013
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| Keywords | 航空宇宙工学 / 航空宇宙流体力学 / 数値流体力学 / 航空機設計 |
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| Research Abstract |
In this study, we developed a conceptual-design-oriented computational fluid dynamics code that is fast and robust. These two factors are required especially during the conceptual design phase of an aircraft. In order to handle an arbitrary complex geometry, Cartesian grid with adaptive mesh refinement is used. Using this grid, compressible Navier-Stokes equations are solve by the program. We have worked constantly on many topics: wall boundary condition treatment (Immersed boundary method), calculation method for force acing on a body, coupling with turbulence model, the development of high-order scheme. Through these development, the code now can be applied to many flow conditions which appears during aircraft designing, such as low-speed flow during take-off and landing, wave drag estimation during super-sonic cruise. Additionally, the code is being extended to the application of unsteady aeroacoustic flow simulation.
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Research Products
(22 results)
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[Presentation]2014
Author(s)
Yoshiharu Tamaki, Taro Imamura
Organizer
3rd AIAA Workshop on Benchmark Problems for Airframe Noise Computations (BANC-III)
Place of Presentation
Atlanta, USA
Year and Date
2014-06-14
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