Flight Tests on U.S.S. Los Angeles. Part II : Stress and Strength Determination (1930)
NASA Technical Reports Server (NTRS) · leaf 9
trifugal forces distributed along the hull. Gages 1 to 12 installed in the forward part of the airship, were the old original gages which had been used in the Shenandoah three years previously. Their records were not sufficiently satisfactory for quantitative measurements. They agreed with the… … Figure 5.—Exterior view of recorder and camera tin4 airship had been flown at the angles of pitch required to offset large inequalities of weight and buoyancy. Figures 6 to 11 and Figure 16 are typical records from the strain gages grouped on the longitudinals around frame 70, as listed in Table…
NASA Technical Reports Server (NTRS)
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