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A System of Load Determination: A Further Step Towards the Development of a Purely Rational Design Process

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1932

Abstract

IN the “Air Commerce Bulletin” issues of November 2 and December 1 (Vol. III, Nos. 9 and 11), reproduced in AIRCRAFT ENGINEERING, February, 1932, pp. 45–49, there appeared articles discussing the possibility of basing aircraft design requirements upon the actual performance of each specific aeroplane type. The programme outlined in those two articles, while fundamentally new, does not represent a radical departure from existing standards, as it is believed advisable to bring about such important changes by progressive stages, if possible.

Citation

(1932), "A System of Load Determination: A Further Step Towards the Development of a Purely Rational Design Process", Aircraft Engineering and Aerospace Technology, Vol. 4 No. 3, pp. 73-75. https://doi.org/10.1108/eb029523

Publisher

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MCB UP Ltd

Copyright © 1932, MCB UP Limited