Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
| Herausgeber (Verlag) | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
| Seitenumfang | 22 |
| ISBN (elektronisch) | 9781624106316 |
| Publikationsstatus | Veröffentlicht - 2022 |
| Veranstaltung | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, USA / Vereinigte Staaten Dauer: 3 Jan. 2022 → 7 Jan. 2022 |
Publikationsreihe
| Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
|---|
Abstract
Future energy-efficient aircraft requires a further drastic reduction in drag and weight. Is it contradictory to improve both at the same time? Is it possible to design a highly efficient HLFC system to be weight-neutral? The present study, performed within the Cluster of Excellence SE2 A – Sustainable and Energy-Efficient Aviation, summarizes aspects and considerations of the contributing disciplines to derive a solution for a suction-based system on short-range aircraft wings with maximum efficiency, i.e. hybrid laminar flow control application capabilities at minimum weight penalty. Several new features – novel wing design and simulation tools, the potentials of thin plies for weigth saving and the 3D-printing possibilities for ventable core structures – are investigated to achive this goal.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
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AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2022. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - The suction panel
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
AU - Wiedemann, Martin
AU - Badrya, Camli
AU - Prasannakumar, Adarsh
AU - Lobitz, Lennart
AU - Traub, Hendrik
AU - Heimbs, Sebastian
AU - Bülow, Christian
AU - Sämann, Philipp
AU - Hühne, Christian
AU - Scheffler, Sven
AU - Brod, Martin
AU - Tariq, Muzzamil
N1 - Funding Information: The authors would like to acknowledge the funding by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany´s Excellence Strategy – EXC 2163/1-Sustainable and Energy Efficient Aviation – Project-ID 390881007 as well as the Helmholtz-Gemeinschaft (HGF) support ExNet-0004-Phase2-3.
PY - 2022
Y1 - 2022
N2 - Future energy-efficient aircraft requires a further drastic reduction in drag and weight. Is it contradictory to improve both at the same time? Is it possible to design a highly efficient HLFC system to be weight-neutral? The present study, performed within the Cluster of Excellence SE2 A – Sustainable and Energy-Efficient Aviation, summarizes aspects and considerations of the contributing disciplines to derive a solution for a suction-based system on short-range aircraft wings with maximum efficiency, i.e. hybrid laminar flow control application capabilities at minimum weight penalty. Several new features – novel wing design and simulation tools, the potentials of thin plies for weigth saving and the 3D-printing possibilities for ventable core structures – are investigated to achive this goal.
AB - Future energy-efficient aircraft requires a further drastic reduction in drag and weight. Is it contradictory to improve both at the same time? Is it possible to design a highly efficient HLFC system to be weight-neutral? The present study, performed within the Cluster of Excellence SE2 A – Sustainable and Energy-Efficient Aviation, summarizes aspects and considerations of the contributing disciplines to derive a solution for a suction-based system on short-range aircraft wings with maximum efficiency, i.e. hybrid laminar flow control application capabilities at minimum weight penalty. Several new features – novel wing design and simulation tools, the potentials of thin plies for weigth saving and the 3D-printing possibilities for ventable core structures – are investigated to achive this goal.
UR - http://www.scopus.com/inward/record.url?scp=85122582759&partnerID=8YFLogxK
U2 - 10.2514/6.2022-0007
DO - 10.2514/6.2022-0007
M3 - Conference contribution
AN - SCOPUS:85122582759
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)
Y2 - 3 January 2022 through 7 January 2022
ER -