The Optimum Design of Long‐Range Aircraft: An Examination of the Best Values of Aspect Ratio Wing Loading and Fuel Load Ratio for Different Conditions
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1957
Abstract
IN the present paper an attempt has been made to determine the optimum aspect ratio, wing loading and fuel load ratio under certain specified design conditions. Aeroplanes with turbojet as well as with airscrew propulsion have been considered.
Citation
Sanders, K.L. (1957), "The Optimum Design of Long‐Range Aircraft: An Examination of the Best Values of Aspect Ratio Wing Loading and Fuel Load Ratio for Different Conditions", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 4, pp. 98-106. https://doi.org/10.1108/eb032813
Publisher
:MCB UP Ltd
Copyright © 1957, MCB UP Limited