NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Evaluation of a Singular Value Decomposition Approach for Impact Dynamic Data CorrelationImpact dynamic tests are used in the automobile and aircraft industries to assess survivability of occupants during crash, to assert adequacy of the design, and to gain federal certification. Although there is no substitute for experimental tests, analytical models are often developed and used to study alternate test conditions, to conduct trade-off studies, and to improve designs. To validate results from analytical predictions, test and analysis results must be compared to determine the model adequacy. The mathematical approach evaluated in this paper decomposes observed time responses into dominant deformation shapes and their corresponding contribution to the measured response. To correlate results, orthogonality of test and analysis shapes is used as a criterion. Data from an impact test of a composite fuselage is used and compared to finite element predictions. In this example, the impact response was decomposed into multiple shapes but only two dominant shapes explained over 85% of the measured response
Document ID
20040014971
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Horta, Lucas G.
(NASA Langley Research Center Hampton, VA, United States)
Lyle, Karen H.
(NASA Langley Research Center Hampton, VA, United States)
Lessard, Wendy B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2003
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-19013
NASA/TM-2003-212657
Report Number: L-19013
Report Number: NASA/TM-2003-212657
Funding Number(s)
OTHER: 762-40-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available