Method uses formulas based on theoretical ideal wing; predicted weight attained by multiplying weight of ideal wing by correction factor derived from statistical analysis of actual wing weights; method provides designer with yardstick by which to compare alternative designs and indicates where improvement might be effected.
Estimation of wing weight
Aircraft Eng
Aircraft Engineering ; 23 , n 267
1951
2 pages
Aufsatz (Zeitschrift)
Englisch
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