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The Aeronautical Journal | Vol.58, Issue.527 | | Pages 765- 768
The Optimum Design of Compression Surfaces having Unflanged Integral Stiffeners
A method is developed enabling rapid determination of the optimum cross-sectional dimensions of compression surfaces having unflanged integral stiffeners, and consideration is given to the effects of practical limitations on the design. The theoretical efficiency of the optimum integral design is found to be only 85 per cent, of that of optimum Z-stringer design.
Original Text (This is the original text for your reference.)
The Optimum Design of Compression Surfaces having Unflanged Integral Stiffeners
A method is developed enabling rapid determination of the optimum cross-sectional dimensions of compression surfaces having unflanged integral stiffeners, and consideration is given to the effects of practical limitations on the design. The theoretical efficiency of the optimum integral design is found to be only 85 per cent, of that of optimum Z-stringer design.
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