Tests made in Langley 4.5-ft flutter research tunnel on uniform, untapered model wing by mounting concentrated weights which were 38, 60, 90 and 100% wing weight; wing was mounted as rigid cantilever; moment of inertia, position of chordwise center of gravity of weight, and spanwise location of weight were varied.
Experimental investigation of effects of concentrated weights on flutter characteristics of straight cantilever wing
Nat Advisory Committee Aeronautics -- Tech Note
1948
39 pages
Report
Englisch
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