The design and stress analysis of an integral land rover structure
Date published
1968-11
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College of Aeronautics
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Report
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Abstract
This report gives in detail the calculation of the distribution of forces in an integral structure by the matrix force method. The design of a full scale structure to test the theoretical results is described in an Appendix but test results will be given in a separate report. The method of analysis is suitable for a small, first generation digital computer and would now be superceded by 'automatic' programs on large computers.