Konrath, Robert and Kirmse, Tania and Kompenhans, Jürgen and Möller, Thorsten J. and Wokoeck, R. and Radespiel, R. (2008) Simultaneous Measurements of Unsteady Aerodynamic Loads, Flow Velocity Fields, Position and Wing Deformations of MAVs in Plunging Motion. 16. DGLR-Fach-Symposium der STAB, 2008-11-03 - 2008-11-04, Aachen, Deutschland.
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Micro Aircraft Vehicles (MAVs) normally operate at very low Reynolds numbers for which existing design methods developed for conventional aircraft are usually not adequate. The performance of airfoils deteriorates rapidly as the Reynolds number decreases below 105. Additionally, the wings of MAVs usually have low aspect ratios of ≤ 2 so that the wing tip vortices influence the overall wing behavior significantly which may result in non-linear characteristics. Because MAVs must be highly maneuverable and are usually very sensitive to gusts, their dynamics and unsteady aerodynamics are of much interest.
|Document Type:||Conference or Workshop Item (Other, Speech)|
|Title:||Simultaneous Measurements of Unsteady Aerodynamic Loads, Flow Velocity Fields, Position and Wing Deformations of MAVs in Plunging Motion|
|In ISI Web of Science:||No|
|Page Range:||p. 2|
|Series Name:||STAB Mitteilung|
|Keywords:||Micro Aircraft Vehicles (MAVs), Flow Velocity Fields|
|Event Title:||16. DGLR-Fach-Symposium der STAB|
|Event Location:||Aachen, Deutschland|
|Event Type:||national Conference|
|Event Dates:||2008-11-03 - 2008-11-04|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Flight Physics|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Experimental Methods|
|Deposited By:||Ilka Micknaus|
|Deposited On:||01 Dec 2008|
|Last Modified:||27 Apr 2009 13:06|
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