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Flutter Investigation ASW-22BL/BLE.

Kießling, F. and Rippl, M. (1994) Flutter Investigation ASW-22BL/BLE. DLR-Interner Bericht. 232 - 94 C 06, 44 S.

Full text not available from this repository.

Abstract

For evaluating flutter proneness of the single-seated high-performance glider ASW-22BL and motor glider ASW-22BLE with 26.4 m wing span manufactured by Alexander Schleicher Segelflugzeugbau GmbH, Poppenhausen, the required investigations according to JAR-22 (Subpart D) 22.629(b)(1) have been conducted. They are based on an additional ground vibration test (ASW-22BLE) and flutter calculations up to 1.2 VD to cover the 26.4 m wing span configurations of the airplane. 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/39649/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Flutter Investigation ASW-22BL/BLE.
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:44
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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