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On simplified Analytical Flutter Clearance Procedures for Light Aircraft.

Kießling, F. (1991) On simplified Analytical Flutter Clearance Procedures for Light Aircraft. Technical Soaring, Vol. XV, pp. 83-91.

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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.

Item URL in elib:https://elib.dlr.de/39472/
Document Type:Article
Additional Information: event_title=OSTIV Sailplane Development Panel, 18.-20. Maerz 1990, Stuttgart, LIDO-Berichtsjahr=1991,
Title:On simplified Analytical Flutter Clearance Procedures for Light Aircraft.
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Journal or Publication Title:Technical Soaring
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
Volume:Vol. XV
Page Range:pp. 83-91
Keywords:Light aircraft, gliders, vibration tests, flutter. Leichtflugzeuge, Segelflugzeuge, Standschwingungsversuch, Flattern.
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: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:44

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