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Additional Flutter Analysis of Sailplane ASW27-18/15

Schwochow, Jan (2006) Additional Flutter Analysis of Sailplane ASW27-18/15. DLR-Interner Bericht. DLR IB-2006 C 10, 65 S.

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Abstract

For evaluating flutter proneness of the glider ASW27-18/15 (manufacturer: Alexander Schleicher GmbH, Poppenhausen/Rhön) the required investigations according to CS-22 (Subpart D) 22.629(B)(1) have been conducted. In this report additional results are summarized for the configuration with extended maximum overall operating mass of 600 kg. Requirements and recommendations are started aiming at a reduction of flutter danger.

Item URL in elib:https://elib.dlr.de/45114/
Document Type:Monograph (DLR-Interner Bericht)
Title:Additional Flutter Analysis of Sailplane ASW27-18/15
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schwochow, JanUNSPECIFIEDUNSPECIFIED
Date:2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:65
Status:Published
Keywords:flutter
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Flexible Aircraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:26 Oct 2006
Last Modified:27 Apr 2009 13:10

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