Holst, H. (1994) Realtime Computation of Wall Shapes in a Two-Dimensional Adaptive Test Section. In: Proceedings 19th ICAS Congress / AIAA Aircraft Systems Conf., Anaheim/CA, USA, 18-23 September 1994, pp. 2738-2753.
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By adapting solely top and bottom flexible walls of a solid-walled test section of rectangular cross section it can be achieved that the wall interferences (Mach number correction, angle of attack correction) are zero along the test section centreline, when testing three-dimensional models. The shapes of the flexible top and bottom walls are determined by the well- known Wedemeyer/Lamarche method of two-dimensional wall adaptation for three-dimensional models. The method performs the wall shape determination in a single computational step, at least when starting from the wall shapes of a preceding Mach number or angle of attack. It uses - in the original computer code of Lamarche - a numerical representation of the necessary mathematical operators. The computing time of 17 seconds on a personal computer could be reduced to 0.3 seconds by using an analytical representation of the operators - following a proposal of E. Wedemeyer. This facilitates the development of a high productivity strategy for wall adaptation in the modernized transonic facility of DLR Goettingen which is equipped with a two-dimensional adaptive test section of 1.0 m x 1.0 m.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Realtime Computation of Wall Shapes in a Two-Dimensional Adaptive Test Section.|
|Journal or Publication Title:||Proceedings 19th ICAS Congress / AIAA Aircraft Systems Conf., Anaheim/CA, USA, 18-23 September 1994|
|Page Range:||pp. 2738-2753|
|Series Name:||ICAS 94 3.8.1|
|Keywords:||Two-Dimensional Wall Adaption, Realtime Computation, Wedemeyer/Lamarche Method, High Productivity|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||L SI - Versuchs- und Simulationstechniken|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||02 Apr 2006|
|Last Modified:||27 Apr 2009 03:28|
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