This paper suggests a means of estimating wing weight using formulae based on the theoretical ideal wing. The predicted wing weight is attained by multiplying the weight of the ideal wing by a correction factor derived from a statistical analysis of actual wing weights. The method has the advantage that it provides the designer with a yardstick by which to compare alternative designs and indicates where improvement might be effected.
The Estimation of Wing Weight
A Method of Predicting Structural Weight by Relating the Design to an Ideal Wing
Aircraft Engineering and Aerospace Technology ; 23 , 5 ; 143-146
1951-05-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft wing weight estimation
Engineering Index Backfile | 1950
|Aircraft Wing Weight Estimation
Emerald Group Publishing | 1950
|Engineering Index Backfile | 1951
|Tilt Rotor Wing Weight Estimation
British Library Conference Proceedings | 1990
|A WING WEIGHT ESTIMATION METHOD BASED ON WING-BOX BEAM DESIGN
TIBKAT | 2020
|