Inside Out Library · Explore
Calculation of wing spars of variable cross-section and linear load (1925)
NASA Technical Reports Server (NTRS) · leaf 5
N.A.C.A, Technical Memorandum 3So.305 Figs.1,2 & 3. cm 2000 Inertia .4050 kg' XQ £j> moments 1000 0 rrrrrr kg 4000 Fig.2 … IV IIINASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Calculation of wing spars of variable cross-section and linear load
More like this
