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
:MCB UP Ltd
Copyright © 1935, MCB UP Limited