Electronic Computers in the Aircraft Industry, File MA 8/8/02. Paper: Bristol Aircraft Ltd. Technical Office Report No. 145. Analysis of Aircraft Structures by the Substructure Relaxation Method by J.S. Przemieniecki, July 1961. Addendum to technical report No. 145. Note on Technical Report No. 145. Paper: Matrix Analysis of Shell Structures with Flexible Frames by J.S. Przemieniecki. November 1958. Paper: The Application of the matrix force method of structural analysis to a typical wing structure by S. Kelsey, Paper No. 38. Various correspondence.
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