Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 242
In con-junction with this hinge a light support, or former, Fig. 152, to which thefabric is attached, is secured to the stabilizer tube every 6 in. by littlelegs. This arrangement reduces the leakage and streamlines the hinge. For main spars which are subjected to torsional stresses in excess…
Airplanes
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