Program System for e* Transition Prediction on Transport Type Wings
Stock, H.W. (1999) Program System for e* Transition Prediction on Transport Type Wings. DLR-Interner Bericht. 129-99/1.
Full text not available from this repository.
The program system consists of three computational methods, which allows to compute in one computational run the transition location in one wing section of large aspect ratio wings (Transport type aircraft). The first method computes the laminar boundary layer development on tapered wings in conical coordinates. The second and third method are e* data base methods for the calculation of the Tollmien-Schlichting instabilities and cross-flow instabilities, respectively. Compared to the computation of the stability data using local, linear stability codes the data base methods need a vanishing fraction of the computational time and moreover ask for almost no engineering effort. The main advantage of the data base methods is due to the fact, that they work fully automatically, which is not feasible applying classical stability codes.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Program System for e* Transition Prediction on Transport Type Wings|
|Keywords:||Program system, 3-D Laminar Flow, e* Transition Prediction, Data base|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ST - Starrflüglertechnologien|
|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:||Claudia Grant|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 20:01|
Repository Staff Only: item control page