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Kießling, F. and Rippl, M. (1994) Flutter Investigation ASW-22BL/BLE. DLR-Interner Bericht. 232 - 94 C 06. 44 S.
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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/ | ||||||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||||||
| Additional Information: | LIDO-Berichtsjahr=1994, | ||||||||||||
| Title: | Flutter Investigation ASW-22BL/BLE. | ||||||||||||
| Authors: |
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| Date: | 1994 | ||||||||||||
| Open Access: | 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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