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.
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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.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||HYLTEC Do 228, Hybrid Laminar Flow Technology Systems, Instrumentation and Flight Test|
|Number of Pages:||40|
|Keywords:||Hybrid Laminar Flow Technology, Boundary Layer Suction, Ice Protection, Contamination Protection, Flight Tests|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L VU - Air Traffic and Environment|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L VU - Air Traffic and Environment|
|DLR - Research theme (Project):||L - Flight Physics|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Configuration Design|
|Deposited By:||Jörg Brüne Meyer|
|Deposited On:||11 Jun 2007|
|Last Modified:||15 Jan 2010 00:49|
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