Zhan, Hao and Streit, Thomas (2002) Design of Multi-Surfaces at Transonic Flow. DLR-Interner Bericht. IB-124-2002/47.
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Abstract
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.
| Item URL in elib: | https://elib.dlr.de/46778/ | ||||||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||||||
| Title: | Design of Multi-Surfaces at Transonic Flow | ||||||||||||
| Authors: |
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| Date: | August 2002 | ||||||||||||
| Refereed publication: | No | ||||||||||||
| Open Access: | No | ||||||||||||
| Status: | Published | ||||||||||||
| 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 (old) | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||
| DLR - Research theme (Project): | L - Flight Physics (old) | ||||||||||||
| Location: | Braunschweig | ||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Configuration Design | ||||||||||||
| Deposited By: | Streit, Dr.rer.nat. Thomas | ||||||||||||
| Deposited On: | 11 Jan 2007 | ||||||||||||
| Last Modified: | 27 Apr 2009 13:24 |
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