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.
Full text not available from this repository.
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)|
|Title:||Comparison of Two Design Codes for Transonic Airfoils.|
|Number of Pages:||95|
|Keywords:||Design Methods, Airfoil Design|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||no assignment|
|HGF - Program Themes:||no assignment|
|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|
Repository Staff Only: item control page