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INTRODUCTION WITH the current trend toward the in crease of the dimensions of aeroplanes, many two‐decked aeroplanes are being designed.
THE purpose of the present report is to present tables and to summarize formulas which are required for the analysis of circular rings, under forces in the plane of the ring or out of the plane. Usually, rings which are redundant structures are calculated by considering strain due to bending only. It is shown that for the stress distribution in a circular ring under given loads, the solution introducing strains due to shearing and axial loads is the same as the solution conventionally used.
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Council, Reports and Technical Notes of the United States National Advisory Committee for Aeronautics and publications of other similar Research Bodies as issued