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11 |
Application of finite elements for computational aeroelasticity
Unger, Ralf. - Göttingen : Cuvillier, 2011, 1. Aufl.
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12 |
Fault investigation and robust failure detection of oscillating aircraft actuation systems using analytical redundancy
Sachs, Helge. - Aachen : Shaker, 2010
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13 |
An adaptive feed-forward controller for active wing bending vibration alleviation on large transport aircraft
Wildschek, Andreas, 2009
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14 |
Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
Cochoy, Olaf. - Aachen : Shaker, 2009
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15 |
A modal control approach based on a minimum order dynamic feedback
Enzinger, Michael Franz. - Aachen : Shaker, 2007
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16 |
Ein modulares Verfahren für die numerische aeroelatische Analyse von Luftfahrzeugen
Braun, Carsten, 2007
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17 |
Nichtlineares Verhalten piezo-elektrisch beeinflußter Strukturen auf der Basis modaler Ansätze
Homann, Stefan. - Köln : DLR, Bibliotheks- und Informationswesen, 2006, Als Ms. gedr.
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18 |
Viscous-inviscid interaction methods for flutter calculations
Sekar, Widjaja Kresna, 2006
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19 |
Updating of local non-linear stiffness- and damping parameters in large order finite elements models by using vibration test data
Böswald, Marc. - Köln : DLR, Bibliotheks- und Informationswesen, 2005, Als Ms. gedr.
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