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Aeroelasticity in Sailplane Design

Schwochow, Jan (2006) Aeroelasticity in Sailplane Design. Technical Soaring, Vol 30 (1-2). ISSN 0744-8996

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Official URL: http://journals.sfu.ca/ts/index.php/ts/index

Abstract

One of many problems in the field of sailplane design is that of aeroelastic stability. Practicing designers of gliders and light aircraft seldom have the opportunity to spend a great deal of time studying the difficult background of flutter. Therefore, the flutter engineers at the Institute of Aeroelasticity are traditionally consulted to test and to certify light aircrafts and gliders for flutter stability. In the following the basics for the mechanism of flutter are presented and the certification process is explained for a representative modern sailplane of the 18m-class starting with the requirements of the Joint Aviation Authorities (JAA). The objectives and methods of the ground vibration test are introduced to measure the vibration properties of the aircraft structure. These data are used to perform the flutter analysis in order to find possible flutter instabilities in the flight envelope. As the maximum flight speed of modern high performance sailplanes is further increased, costly modifications of the prototype are often necessary to satisfy a safe design. Therefore, a method is presented to estimate the flutter behavior during the design process.

Item URL in elib:https://elib.dlr.de/84247/
Document Type:Article
Title:Aeroelasticity in Sailplane Design
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schwochow, Janjan.schwochow (at) dlr.deUNSPECIFIED
Date:1 January 2006
Journal or Publication Title:Technical Soaring
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol 30
Editors:
EditorsEmail
Milgram, Judahmilgram@cgpp.com
ISSN:0744-8996
Status:Published
Keywords:aeroelasticity, flutter, ground vibration test
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Experiments
Deposited By: Schwochow, Jan
Deposited On:25 Sep 2013 14:30
Last Modified:25 Sep 2013 14:30

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