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Some Specific Challenges of HLFC Design on a Long-range Wing

Schrauf, Geza and Kilian, Thomas (2023) Some Specific Challenges of HLFC Design on a Long-range Wing. In: New Results in Numerical and Experimental Fluid Mechanics XIV, 23nd STAB/DGLR Symposium 2022 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 16. Springer. ISSN 1612-2909.

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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/193840/
Document Type:Contribution to a Collection
Title:Some Specific Challenges of HLFC Design on a Long-range Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schrauf, GezaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kilian, ThomasUNSPECIFIEDhttps://orcid.org/0000-0003-1395-608XUNSPECIFIED
Date:2023
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics XIV, 23nd STAB/DGLR Symposium 2022
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:16
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Heller, GerdAirbus BremenUNSPECIFIEDUNSPECIFIED
Krämer, EwaldInstitut für Aerodynamik und Gasdynamik Universität StuttgartUNSPECIFIEDUNSPECIFIED
Wagner, ClausUNSPECIFIEDhttps://orcid.org/0000-0003-2273-0568UNSPECIFIED
Weiss, JulienTU BerlinUNSPECIFIEDUNSPECIFIED
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
Status:Accepted
Keywords:Hybrid Laminar Flow Control (HLFC), suction system design, variable microperforation, A320 VTP, HLFC wing
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:17 May 2023 09:50
Last Modified:17 May 2023 09:50

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