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Comparison of Two Design Codes for Transonic Airfoils.

Hua, J. (1) and Köster, H. (1990) Comparison of Two Design Codes for Transonic Airfoils. DLR-Interner Bericht. 129-90/36, 95 S.

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Abstract

Within the framework of DLR-CAE cooperation two design codes for transonic airfoils are exchanged. The first method is developed at NPU, Xian, China, and based on the iterative residual correction concept; the second one is a DLR modification of the artificial viscosity method of McFadden. Parameter investigations with both methods have been carried out,several different design examples have been performed. The results are compared and show that both methods are equally capable in designing transonic airfoils.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1990,
Title:Comparison of Two Design Codes for Transonic Airfoils.
Authors:
AuthorsInstitution or Email of Authors
Hua, J. (1)UNSPECIFIED
Köster, H.UNSPECIFIED
Date:1990
Number of Pages:95
Status:Published
Keywords:Design Methods, Airfoil Design
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:04

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