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Results of full-scale Helicopter Drop Test 2 - Proposals for Drop Test 3

Lützenburger, Marius (2007) Results of full-scale Helicopter Drop Test 2 - Proposals for Drop Test 3. DLR-Interner Bericht, Project Report. DLR-IB 435-2007/25, 27 S. (Unpublished)

Full text not available from this repository.

Abstract

Within the EU funded project HeliSafe TA (2004 – 2007), three helicopter drop tests were carried out at CIRA’s test facility LISA. Bell UH-1D helicopters were used in all tests. DLR carried out an extensive evaluation of the drop test results – using the videos and data provided by CIRA as well as the measurements from SRS: The times of the most important occurrences in the drop tests were identified. The events were ordered chronologically and given in 3 different time scales (CIRA, SRS and a scale which uses the moment of the first impact as T = 0 s). Furthermore, DLR developed a data evaluation process which allows • The verification of accelerometer signals • The detection of interchanged signals (X, Z => Z, X) • The calculation of the exact orientation of each accelerometer before the impact • The calculation of the oscillation of the helicopter (change of pitch angle) before the impact The document also includes some proposals for the third drop test, e.g. the change of certain accelerometers positions and suggestions for the position of clinometers. Another proposal is related to the measurement of the helicopter release velocity.

Item URL in elib:https://elib.dlr.de/52583/
Document Type:Monograph (DLR-Interner Bericht, Project Report)
Title:Results of full-scale Helicopter Drop Test 2 - Proposals for Drop Test 3
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lützenburger, MariusUNSPECIFIEDUNSPECIFIED
Date:24 August 2007
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:27
Status:Unpublished
Keywords:helicopter crash test, accelerometer
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Robust Rotorcraft (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Structural Integrity
Deposited By: Lützenburger, Marius
Deposited On:07 Jan 2008
Last Modified:27 Apr 2009 14:36

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