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.
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/eb029978Download as .RIS
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