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Hybrid Laminar Flow Control on A320 Fin: Retrofit Design and Sample Results

Schrauf, Geza and von Geyr, Heiko (2021) Hybrid Laminar Flow Control on A320 Fin: Retrofit Design and Sample Results. Journal of Aircraft, 58 (6), pp. 1272-1280. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C036179. ISSN 0021-8669.

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Abstract

A flight test with a simplified hybrid laminar flow control (HLFC) system on the vertical tail plane (VTP) of an A320 aircraft was performed in April/May 2018. This HLFC system was a prototype for a simplified system that might be attractive for drag reduction of commercial long-range aircraft. The paper presents the design principles of a simplified HLFC system, including passive suction, and shows their application to aerodynamic and suction system design for the retrofit of an A320 VTP. Furthermore, sample flight test results will be presented and discussed.

Item URL in elib:https://elib.dlr.de/146436/
Document Type:Article
Title:Hybrid Laminar Flow Control on A320 Fin: Retrofit Design and Sample Results
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schrauf, GezaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
von Geyr, HeikoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:November 2021
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:58
DOI:10.2514/1.C036179
Page Range:pp. 1272-1280
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:Hybrid Laminar Flow Control, Laminar-Turbulent Transition, Boundary Layer Suction, Drag Reduction, e^N Method, Flight Test, Linear Stability Theory
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 - Virtual Aircraft and  Validation
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schrauf, Geza
Deposited On:09 Dec 2021 08:18
Last Modified:24 May 2022 23:47

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