Electronic computers in the aircraft industry, file MA 8/8/02. Paper: The application of a matrix force method of structural analysis to a typical wing structure by S. Kelsey, paper No. 38. Paper : Kron's technique and the flexibility matrix by J.M Bennett. Note on Bristol Technical Office Report No. 145, Ref: 824/ICT/SS/468. Report: Bristol Aircraft Ltd. Addendum to Technical Office Report No. 145. Numerical example on the substructure relaxation method by J.S. Przemieniecki, FW/SDO/6/2287.Technical office report No. 145, Analysis of aircraft structures by the substructure relaxation method by J.S. Przemieniecki. Report: Vickers-Armstrongs Ltd. Influence Coefficients for a Simple Beam from Engineers Theory, VTO/M/383. Report: Sir W.G.Armstrong Whitworth Aircraft Ltd. Ref. ARM6/GAC/19.13.3, Preliminary notes on the Evaluation of Pressure Distribution and Flutter Derivatives for a Wing of Arbitrary Planform at Supersonic Speeds (Zero Frequency) by J. Perry. Report: A.V. Roe Co. Ltd. Electronics /32 Stability and Response Calculations on a Digital Computer, prepared by A. Wragg. Paper: Matrix Analysis of Shell Structures with Flexible Frames by J.S. Przemieniecki. reprinted from The Aeronautical Quarterly, Vol. IX, November 1958. List of papers presented to S.B.A.C. Electronic Computer Panels.