Investigation made to obtain experimental data on amount of gust load alleviation that might be expected as result of wings flexing under load; results indicated that unless adverse pitching motion could be eliminated or reduced, overall load reduction would be small; net reduction in bending moment, however, may be appreciable.
Gust-tunnel investigation of flexible-wing model with semichord line swept back 45°
Nat Advisory Committee Aeronautics -- Tech Note
1949
13 pages
Illus, Diagrs, Charts, Tables
Report
Englisch
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