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Flutter Investigation DG 800S Sailplane.

Kießling, F. and Rippl, M. (1994) Flutter Investigation DG 800S Sailplane. DLR-Interner Bericht. 232 - 94 C 07, 73 S.

Full text not available from this repository.

Abstract

For evaluating flutter proneness of the single-seat high-performance sailplane DG-800S, manufactured by Glaser-Dirks Flugzeugbau, Bruchsal, the required investigations according to JAR-22 (Subpart D) 22.629(b)(1) have been conducted. This report deals with both the 18 m span version and the 15 m span version with winglets. A ground vibration test and flutter calculations up to 1.2 VD covering all configurations of the airplane have been performed. The significant results are summarized in this report. Requirements and recommendations are stated aiming at a reduction of flutter risk.

Item URL in elib:https://elib.dlr.de/39651/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Flutter Investigation DG 800S Sailplane.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kießling, F.UNSPECIFIEDUNSPECIFIED
Rippl, M.UNSPECIFIEDUNSPECIFIED
Date:1994
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:73
Status:Published
Keywords:aeroelasticity, ground vibration test, flutter analysis.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
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 10:50

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