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Aeroplane Loading Conditions: A Method of Presenting the Conditions by Means of a Simple Chart

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1935

Abstract

IT is well known that the loading of aeroplanes is required to conform with certain design limits of C.G. travel and maximum permissible weight, which are governed by aerodynamic requirements.

Citation

Osborne, S.P. (1935), "Aeroplane Loading Conditions: A Method of Presenting the Conditions by Means of a Simple Chart", Aircraft Engineering and Aerospace Technology, Vol. 7 No. 10, pp. 259-260. https://doi.org/10.1108/eb029978

Publisher

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MCB UP Ltd

Copyright © 1935, MCB UP Limited