Computational method estimates weight of aircraft wings from theoretical relationships and empirical data. Permits comparison of alternative materials, methods of construction, and design philosophies. Method used to make tradeoffs in preliminary design phases on basis of simple input data and for more accurate calculations in later phases when more data are available.
Semiempirical Estimate of Aircraft Wing Weight
NASA Tech Briefs ; 7 , 1
1983-03-01
Sonstige
Keine Angabe
Englisch
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