The determination of the effective mass and moment of inertia of a pendulum impactor
van Huffelen, Rolf and Zipfel, Ary and Baaran, Jens (2004) The determination of the effective mass and moment of inertia of a pendulum impactor. DLR-Interner Bericht. DLR-IB 131-2004/01, 19 S.
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Impact tests can be performed by using a drop weight or a pendulum as is being done within the DLR. In order to simulate the impact tests within the CODAC program it is necessary to know the effective mass and velocity of the impactor head. If a drop weight is being used the effective mass equals the weight’s mass, in case of a pendulum the effective mass has to be calculated.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||The determination of the effective mass and moment of inertia of a pendulum impactor|
|Number of Pages:||19|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems|
|Deposited By:||Doris Ries|
|Deposited On:||26 Jun 2007|
|Last Modified:||27 Apr 2009 13:53|
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