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Structural Integrity Assurance of Aerospace Vehicles
Department of Mechanical Engineering
University of Maine
Funded by the Maine Space Grant Consortium
in cooperation with the NASA Johnson Space Center, Houston, TX
Contents
1. Introduction and Objectives
2. Modal Analysis – Tap Testing
2.2 Panel Weight
2.3 Experimental Setup
2.4 Modal Testing
3. Finite Element Analysis
and Experimental Correlation
3.1 Material Properties
3.2 Mass
3.3 Non-Tiled Honeycomb Panel
3.4 Tiled Honeycomb Panel
4 Conclusions
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This is an official publication of the University of Maine Send comments to grant@umeme.maine.edu |