Force variation along wing span under combined normal and angular accelerations considered; required aerodynamic load distributions obtained by use of wing theory and wing inertia distributions are based on analysis of wing weight data; several examples included to illustrate effect of wing taper and aileron span on total shears and moments at any section along span.
Study of unsymmetrical-loading conditions
Nat Advisory Committee Aeronautics -- Tech Note
1940
34 pages
12 Supp sheets, Bibliography
Report
Englisch
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A study of unsymmetrical-loading conditions
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