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Schrauf, Geza and Kilian, Thomas (2023) Some Specific Challenges of HLFC Design on a Long-Range Wing. In: 23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV Notes on Numerical Fluid Mechanics and Multidisciplinary Design., 154. Springer Nature Switzerland AG. pp. 382-391. doi: 10.1007/978-3-031-40482-5_36. ISSN 1612-2909.
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Official URL: https://www.tu.berlin/aero/stab-symposium-2022
Abstract
We describe the aerodynamic design of an HLFC system for the wing of a large transport aircraft and compare it to the the HLFC system installed in the VTP of the DLR A320 ATRA aircraft. For the VTP we used the ALTTA-design with a laser-drilled microperforated titanium sheet with only one microperforation and small suction chambers beneath it. For the wing we designed a system with only one large plenum and controlled the suction with the help of variable microperforation. Some specific challenges of an HLFC design on a wing in contrast to a VTP application are highlighted here.
| Item URL in elib: | https://elib.dlr.de/198026/ | ||||||||||||||||||||||||
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| Document Type: | Contribution to a Collection | ||||||||||||||||||||||||
| Additional Information: | The A320 flight test activities received funding from the European Community’s Seventh Framework Programme FP7/2007-2013, under grant agreement no 604013, AFLoNext project. The HLFC-WIN project received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement CS2-LPA-GAM-2020-2023-01. The JU receives support from the European Union’s Horizon 2020 research and innovation programme and Clean Sky 2 JU members not in the Union. | ||||||||||||||||||||||||
| Title: | Some Specific Challenges of HLFC Design on a Long-Range Wing | ||||||||||||||||||||||||
| Authors: |
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| Date: | 2023 | ||||||||||||||||||||||||
| Journal or Publication Title: | 23rd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIV | ||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||
| Volume: | 154 | ||||||||||||||||||||||||
| DOI: | 10.1007/978-3-031-40482-5_36 | ||||||||||||||||||||||||
| Page Range: | pp. 382-391 | ||||||||||||||||||||||||
| Editors: |
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| Publisher: | Springer Nature Switzerland AG | ||||||||||||||||||||||||
| Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design. | ||||||||||||||||||||||||
| ISSN: | 1612-2909 | ||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||
| Keywords: | HLFC, Laminar wing design | ||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||
| HGF - Program Themes: | Efficient Vehicle | ||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||
| DLR - Program: | L EV - Efficient Vehicle | ||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Aircraft Technologies and Integration | ||||||||||||||||||||||||
| Location: | Braunschweig | ||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Transport Aircraft | ||||||||||||||||||||||||
| Deposited By: | Kilian, Thomas | ||||||||||||||||||||||||
| Deposited On: | 06 Dec 2023 12:47 | ||||||||||||||||||||||||
| Last Modified: | 12 Dec 2023 09:48 |
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