Influence of Loss of Laminarity on the Aerodynamic Characteristics of the NLF F100 Airfoil.
Redeker, G. (1996) Influence of Loss of Laminarity on the Aerodynamic Characteristics of the NLF F100 Airfoil. DLR-Interner Bericht. 19101-96C01, 72 S.
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From the geometry of the laminar glove of the Fokker F100 a two-dimensional wing section has been derived. For various flow conditions (M- and Re-number) the influence of loss of laminarity on the airfoil performance has been studied numerically by considering different chordwise positions of the transition locations. The most remarkable result was that the airfoil drag was increased by more than a factor of 2, when the airfoil lost completely its laminar boundary layers.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Influence of Loss of Laminarity on the Aerodynamic Characteristics of the NLF F100 Airfoil.|
|Number of Pages:||72|
|Keywords:||Laminar airfoils, loss of laminarity.|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||02 Apr 2006|
|Last Modified:||27 Apr 2009 05:29|
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