Zhan, Hao and Streit, Thomas (2002) Design of Multi-Surfaces at Transonic Flow. DLR-Interner Bericht. IB-124-2002/47.
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A transonic multi-lifting surface design method coupled with CFD tools and programs is used for the design of a canard/wing configuration. The aerodynamic design method for a single lifting surface based upon the iterative residual correction principle is developed for designing mult-lifting surfaces, an aerodynamic design code based on this method is extended and coupled with the advanced aerodynamic analysis codes in order to be able to design multi-lifting surfaces. Using such an aerodynamic design software system, a canard/wing configuration is studied and designed. The method and software developed within this work has significant practical value for aircraft design.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Design of Multi-Surfaces at Transonic Flow|
|In ISI Web of Science:||No|
|Keywords:||inverse design, multi-lifting surface design method, two surface aircraft, residual correction method, CFD-RANS|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Flight Physics|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Configuration Design|
|Deposited By:||Dr.rer.nat. Thomas Streit|
|Deposited On:||11 Jan 2007|
|Last Modified:||27 Apr 2009 13:24|
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