Summary of Flow Modulation and Fluid-Structure Interaction Findings : Results of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008

The Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program...

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Chi tiết về thư mục
Tác giả khác: Schröder, Wolfgang, 19..-...., chercheur en mécanique des fluides (Giám đốc xuất bản)
Định dạng: Livre numérique
Ngôn ngữ:Anglais
Được phát hành: Berlin, Heidelberg : Springer Berlin Heidelberg [20..].
Cham : Springer Nature
Phiên bản:1st ed. 2010.
Loạt:Notes on Numerical Fluid Mechanics and Multidisciplinary Design 109
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Accès Université d'Orléans
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Chú thích: Archives Springer e-books (Licence nationale)
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Edition sous un autre format:• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040962
• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642263729
• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040870
• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040962
• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642263729
• Summary of Flow Modulation and Fluid-Structure Interaction Findings, Texte imprimé, 9783642040870
Miêu tả
Tóm tắt:The Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.
Mô tả sách:Archives Springer e-books (Licence nationale)
Archives Springer e-books (Licence nationale)
số ISBN:9783642040887
số ISSN:1860-0824
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