By Dietrich Knörzer (auth.), Prof. Dr.-Ing. Peter Thiede (eds.)
------------------------------------------------------------ This quantity comprises the lawsuits of the CEAS/DragNet eu Drag relief convention hung on 19-21 June 2000 in Potsdam, Germany. This convention, succeeding the ecu Fora on Laminar move know-how 1992 and 1996, was once initiated via the ecu Drag relief community (DragNet) and organised through DGLR less than the auspice of CEAS. The convention addressed the hot advances in all components of drag relief learn, improvement, validation and demonstration together with laminar circulate know-how, adaptive wing innovations, turbulent and caused drag aid, separation keep an eye on and supersonic move facets. This quantity which includes greater than forty convention papers is of specific curiosity to engineers, scientists and scholars operating within the aeronautics undefined, study institutions or academia.
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Additional info for Aerodynamic Drag Reduction Technologies: Proceedings of the CEAS/DragNet European Drag Reduction Conference, 19–21 June 2000, Potsdam, Germany
4. 2. 5. Energy Sources Instrumentation 3. 6. Systems Certification At the time of writing, the concept and design stages of this project have been completed. st: leading edges is part completed as is the provision of test equipment, energy sources and other modifications to the aircraft. 4 CONCEPTUAL ARRANGEMENT Figure I illustrates the test aircraft and was taken during a previous, unrelated, laminar flow campaign. However, for this test, the same pod mounted infra-red boundary layer imaging system will be used and a laminar flow glove will be installed similar to the one that can be seen on the right wing.
Let us recall that ONERA and DLR have now a common yearly Symposium ODAS (ONERA-DLR Aerospace Symposium). The second one took place in Berlin last week. ONERA and DLR have also a common scientific journal AST (Aerospace Science and Technology) published by Elsevier, in which other RE participate. But this only involves two research establishments. The true challenge is to join all European forces. And in this respect I would like to say a few words about EREA, which is certainly well known by all of you, but which has recently experienced important changes you may not be aware of.
A more sophisticated approach is to vary the suction rate and to examine the movement of transition: as the mean suction velocity increases, the transition mechanism changes suddenly from CF-induced to TS-induced, much further aft on the wing. This leads to a recommended suction rate which is just sufficient to push transition aft to the mid-chord region. Figure 3 shows how, with a transition N-factor of 9, this can be achieved with much less suction (about half) than that required for the complete stabilisation of CF modes.
Aerodynamic Drag Reduction Technologies: Proceedings of the CEAS/DragNet European Drag Reduction Conference, 19–21 June 2000, Potsdam, Germany by Dietrich Knörzer (auth.), Prof. Dr.-Ing. Peter Thiede (eds.)