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On Simplified Analytical Flutter Clearance Procedures for Light Aircraft.

Kießling, F. (1990) On Simplified Analytical Flutter Clearance Procedures for Light Aircraft. OSTIV Sailplane Development Panel, 18-20 March, Stuttgart.

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Abstract

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)
Additional Information: LIDO-Berichtsjahr=1990,
Title:On Simplified Analytical Flutter Clearance Procedures for Light Aircraft.
Authors:
AuthorsInstitution or Email of Authors
Kießling, F.UNSPECIFIED
Date:1990
Status:Published
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
Location: Göttingen
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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