Lüdeke, Heinrich and Viola, Wartemann (2011) DNS of Mack-Mode Damping on Porous Coated Cones. 4th European Conference for Aerospace Sciences, 4.-8. Jul. 2011, St. Petersburg, Russland.
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The flow field over a 3° blunt cone is investigated with respect to a hypersonic stability analysis of the boundary-layer flow at Mach 6 with and without porous walls by comparing local DNS and LST data. The original boundary-layer profile is generated by a finite volume solver, using shock capturing techniques to generate an axisymmetric flow field. Local boundary-layer profiles are extracted from this flow field and hypersonic Mack-modes are superimposed for cone-walls with- and without a porous surface, used as a passive transition-reduction device. Special care is taken on curvature effects of the wall on the mode development over smooth and porous walls.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||DNS of Mack-Mode Damping on Porous Coated Cones|
|Date:||4 July 2011|
|In ISI Web of Science:||No|
|Keywords:||kegelströmung, DNS, Mack Moden, poröse Oberflächen, Transition|
|Event Title:||4th European Conference for Aerospace Sciences|
|Event Location:||St. Petersburg, Russland|
|Event Type:||international Conference|
|Event Dates:||4.-8. Jul. 2011|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||Space Transport|
|DLR - Research area:||Raumfahrt|
|DLR - Program:||R RP - Raumtransport|
|DLR - Research theme (Project):||R - Projekt IMENS-3C (old)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Spacecraft|
|Deposited By:||Dr.-Ing. Heinrich Lüdeke|
|Deposited On:||17 Nov 2011 09:00|
|Last Modified:||08 May 2014 23:17|
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