elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Aeroelastic Flutter Prevention in Gliders and Small Aircraft.

Stender, W. and Kießling, F. (1990) Aeroelastic Flutter Prevention in Gliders and Small Aircraft. DLR-Interner Bericht. 232-90 J 10, 60 S.

Full text not available from this repository.

Abstract

An empirical method is specified which can be used by the manufacturers of gliders and small aircraft to evaluate flutter vulnerability without extensive computational analysis and to take appropriate preventive measures. Suggestions are given on how designers can avert flutter from the very outset of the designing process. This method has been applied by the author in numerous cases and can be considered proven for conventional structures. It is based on the results of a simple vibration test as well as stiffness and friction measurements taken on the control surfaces is derived. Simple formulas for the calculation of the torsion frequency and the critical speed for torsional flutter are given.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1990,
Title:Aeroelastic Flutter Prevention in Gliders and Small Aircraft.
Authors:
AuthorsInstitution or Email of Authors
Stender, W.UNSPECIFIED
Kießling, F.UNSPECIFIED
Date:1990
Number of Pages:60
Status:Published
Keywords:Vibrations, Flutter, Glider, Small Aircraft, Mass Balance
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

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.