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HYLTEC Do 228, Hybrid Laminar Flow Technology Systems, Instrumentation and Flight Test

Meyer, Jörg Brüne and Horstmann, Karl Heinz and de Groot, Klaus and Krückeberg, Claus-Peter and Sitzmann, Martin and Weddig, Thomas (2007) HYLTEC Do 228, Hybrid Laminar Flow Technology Systems, Instrumentation and Flight Test. DLR-Interner Bericht. DLR-IB 124-2007/904, 40 S.

Full text not available from this repository.

Abstract

Hybrid Laminar Flow Control consisting of interacting sub-systems for boundary layer suction, contamination and ice protection has been the subject of flight tests with the DLR Do228 test vehicle in 2002 as Task 1.1.4 in the EC founded HYLTEC (Hybrid Laminar Flow Technology) Project. In this contribution a description of system layout and flight test results is given. The HYLTEC flight tests clearly demonstrated that protection systems against icing and insect contamination can be successfully integrated into a boundary layer suction system.

Item URL in elib:https://elib.dlr.de/48795/
Document Type:Monograph (DLR-Interner Bericht)
Title:HYLTEC Do 228, Hybrid Laminar Flow Technology Systems, Instrumentation and Flight Test
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Meyer, Jörg BrüneUNSPECIFIEDUNSPECIFIED
Horstmann, Karl HeinzUNSPECIFIEDUNSPECIFIED
de Groot, KlausUNSPECIFIEDUNSPECIFIED
Krückeberg, Claus-PeterUNSPECIFIEDUNSPECIFIED
Sitzmann, MartinUNSPECIFIEDUNSPECIFIED
Weddig, ThomasUNSPECIFIEDUNSPECIFIED
Date:May 2007
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:40
Editors:
EditorsEmail
DLR-AS, UNSPECIFIED
Keywords:Hybrid Laminar Flow Technology, Boundary Layer Suction, Ice Protection, Contamination Protection, Flight Tests
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Configuration Design
Deposited By: Meyer, Jörg Brüne
Deposited On:11 Jun 2007
Last Modified:15 Jan 2010 00:49

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