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Design of Multi-Surfaces at Transonic Flow

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.

Document Type:Monograph (DLR-Interner Bericht)
Title:Design of Multi-Surfaces at Transonic Flow
Authors:
AuthorsInstitution or Email of Authors
Zhan, HaoNorthwestern Polytechnical University, Xi'an, China
Streit, ThomasUNSPECIFIED
Date:August 2002
Refereed publication:No
In SCOPUS:No
In ISI Web of Science: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
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Braunschweig
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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