Abstract
Today it is often discussed whether the performance of a modern transport aircraft in the usual wing-body configuration can be further increased at all, or whether its curve over time has reached an asymptotic stadium.
During the presentation of this paper in the 1St European DragNet Conference in Potsdamm 2000, the video about this programme has been presented, called “A Nose Ahead”.
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Reference
R. Henke: The: The “A 320 HLF Fin Programme”: Objectives and Challenges CEAS 2“d European Forum on Laminar Flow Technology, Bordeaux, June 1996
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© 2001 Springer-Verlag Berlin Heidelberg
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Henke, R. (2001). Airbus A 320 HLF Fin Flight Tests. In: Thiede, P. (eds) Aerodynamic Drag Reduction Technologies. Notes on Numerical Fluid Mechanics (NNFM), vol 76. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_4
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DOI: https://doi.org/10.1007/978-3-540-45359-8_4
Publisher Name: Springer, Berlin, Heidelberg
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