Lüdeke, Heinrich (2018) Numerical Investigation of TS-Wave Growth Over Surface-Steps on a Laminar Profile with Suction. ECCM - ECFD 2018 Conference, 2018-06-11 - 2018-06-15, Glasgow, UK.
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Kurzfassung
The aerodynamic design of laminar profiles with suction is generally carried out by Linear Stability Theory (LST) as a quick and reliable prediction-tool for the transition-position. Alternatives, like direct simulations of transitional modes, have shown promising results for the understanding of the scientific background under special flow-conditions, for cases where basic assumptions of classic LST are violated. A typical geometric singularity of this class, is the forward- or backward facing step, violating the parallel-flow assumption at corners that require a special singularity-treatment, as demonstrated by Zahn and Rist. For Tollmien-Schlichting (TS) modes, a two-dimensional approach of the perturbed boundary-layer flow-field is not very time-consuming and allows the investigation of TS-modes over even complicated geometries, including the non-linear growth effects. Future experiments on the laminar leading-edge of a vertical-tail model are planned with suction-panels for Hybrid Laminar Flow Control (HLFC) by sealing two suction panels with a thin tape, resulting in additional forward- and backward facing steps. Laminar flow-stabilization by suction is expected in front and downstream the taped region. Especially the backward facing-step shows strongly destabilizing influences on the TS-modes. The character of the dominating TS-waves allows 2D simulations of the flow-field by using a well-validated high-order numerical approach which will be sufficient for a detailed simulation of transitional modes in the region of interest. To demonstrate sufficient transition suppression by the suction-panel with or without sealing-tape, direct numerical simulations of critical TS-modes are planned, including post-processing and comparison with growth-rates on unperturbed surfaces and stabilization by uniform suction. The strong stabilizing effect of such approaches was already successfully calculated by Rist and Zahn.
elib-URL des Eintrags: | https://elib.dlr.de/124604/ | ||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||
Titel: | Numerical Investigation of TS-Wave Growth Over Surface-Steps on a Laminar Profile with Suction | ||||||||
Autoren: |
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Datum: | 11 Juni 2018 | ||||||||
Referierte Publikation: | Ja | ||||||||
Open Access: | Nein | ||||||||
Gold Open Access: | Nein | ||||||||
In SCOPUS: | Nein | ||||||||
In ISI Web of Science: | Nein | ||||||||
Status: | veröffentlicht | ||||||||
Stichwörter: | HLFC, DNS, Transition, Suction, Surface-perturbation | ||||||||
Veranstaltungstitel: | ECCM - ECFD 2018 Conference | ||||||||
Veranstaltungsort: | Glasgow, UK | ||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||
Veranstaltungsbeginn: | 11 Juni 2018 | ||||||||
Veranstaltungsende: | 15 Juni 2018 | ||||||||
Veranstalter : | Eccomas | ||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
HGF - Programm: | Luftfahrt | ||||||||
HGF - Programmthema: | Flugzeuge | ||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt) | ||||||||
Standort: | Braunschweig | ||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge | ||||||||
Hinterlegt von: | Lüdeke, Dr.-Ing. Heinrich | ||||||||
Hinterlegt am: | 13 Dez 2018 14:43 | ||||||||
Letzte Änderung: | 24 Apr 2024 20:28 |
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