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Volume 29, Issue 4
1 April 1957
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 29, Issue 4
Review Article| April 01 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 Available to Purchase

Karl L. Sanders
Karl L. Sanders
Design Engineer at I.A.M.E. Institute Aerotecnico, Cordoba, Argentina.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1957
Aircraft Engineering (1957) 29 (4): 98–106.
https://doi.org/10.1108/eb032813

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.

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© MCB UP Limited
1957
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