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Simplified Hybrid Laminar Flow Control for the A320 Fin Aerodynamic and System Design - First Results

Schrauf, Geza and von Geyr, Heiko (2020) Simplified Hybrid Laminar Flow Control for the A320 Fin Aerodynamic and System Design - First Results. AIAA Science and Technology Forum and Exhibition - SCITECH, 6.-10. Jan. 2020, Orlando, Florida, USA. DOI: 10.2514/6.2020-1536

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Abstract

A flight test with a simplified HLFC system on the vertical tail plane of an A320 aircraft was performed in April/May 2018. The aerodynamic and system design is discussed and first results of the flight tests are presented.

Item URL in elib:https://elib.dlr.de/133922/
Document Type:Conference or Workshop Item (Speech)
Title:Simplified Hybrid Laminar Flow Control for the A320 Fin Aerodynamic and System Design - First Results
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schrauf, GezaGeza.Schrauf (at) dlr.deUNSPECIFIED
von Geyr, HeikoHeiko.vGeyr (at) dlr.deUNSPECIFIED
Date:January 2020
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2020-1536
Status:Published
Keywords:Flight Test, A320 VTP, Drag Reduction, Hybrid Laminar Flow Control, Boundary Layer Suction
Event Title:AIAA Science and Technology Forum and Exhibition - SCITECH
Event Location:Orlando, Florida, USA
Event Type:international Conference
Event Dates:6.-10. Jan. 2020
Organizer:American Instutute of Aeronautics and Astronautics (AIAA)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schrauf, Geza
Deposited On:29 Jan 2020 09:14
Last Modified:29 Jan 2020 09:14

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