Kießling, F. (1990) On Simplified Analytical Flutter Clearance Procedures for Light Aircraft. OSTIV Sailplane Development Panel, 18-20 March, Stuttgart.
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For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter analyses which are necessary for high-performance civil and military aircraft types. A specific procedure is accepted in Germany which is based on a more or less simplified ground vibration test and - depending on the test results - a statistical evaluation of flutter danger or stability calculations. Together with flight tests conducted by the manufacturer, the analytical findings constitute the conditions of flutter clearance. Experiences in applying this concept are presented in this report.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||On Simplified Analytical Flutter Clearance Procedures for Light Aircraft.|
|Keywords:||Leichtflugzeuge, Segelflugzeuge, Standschwingungsversuch, Flattern|
|Event Title:||OSTIV Sailplane Development Panel, 18-20 March, Stuttgart|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||other|
|HGF - Program Themes:||other|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||no assignment|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Aeroelasticity|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||02 Apr 2006|
|Last Modified:||27 Apr 2009 10:42|
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