The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique coordinates
Date published
1951-04
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College of Aeronautics, Cranfield.
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Report
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Abstract
This report is an addition to the college of Aeronautic Report No. 31. The purpose of the report is to enable one to obtain the matrix elements used in the analysis of swept-back wing structures by oblique coordinated in a very rapid manner.