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Flutter Flight Test of the Ranger 2000 Aircraft

Hönlinger, H. and Schweiger, J. and Weiß, F. (1995) Flutter Flight Test of the Ranger 2000 Aircraft. AGARD CP 566 Meeting, May 1995.

Full text not available from this repository.

Abstract

The philosophy of a comprehensive flight flutter test using rotating vane exciter and pulse excitation is outlined. Based on the results of the flutter analysis, a lean flight test program was developed and dedicated to wing and T-tail investigations in areas of the flight envelope where low damping was predicted. The implementation of the rotating vane exciter system was well as the sensor installation is described. Emphasis is put on reporting the flight test performance, excitation techniques and quasi online data evaluation. Comparison of test results with analysis is presented.

Item URL in elib:https://elib.dlr.de/39786/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Flutter Flight Test of the Ranger 2000 Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hönlinger, H.UNSPECIFIEDUNSPECIFIED
Schweiger, J.DASAUNSPECIFIED
Weiß, F.DASAUNSPECIFIED
Date:1995
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:flight flutter testing, vane exciter, pulse excitation, lean flight test program, wing and T-tail investigations
Event Title:AGARD CP 566 Meeting, May 1995
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
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 10:54

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