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.
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 ; 29 , 4 ; 98-106
01.04.1957
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Optimum design of long-range aircraft
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