Flight Tests on U.S.S. Los Angeles. Part II : Stress and Strength Determination (1930)
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P) — 35 (2P) Figure 6.—Camera No. 1. Run No. 4 Figures 12 to 15, inclusive, are the records of the gages extended longitudinally along the bottom of the airship as recorded in Table II. Only Figure 15 of this group is of much sig- 25 (2%S) 26 (2%5) 27 (2SJ 28 MS/ 29 (i'/gSJ 30 $SJ 31 (KP) 32 (%P)… … Figure 16 is typical of the large stresses during the rough air of the first day of the trials. This record was not synchronized with the N. A. C. A. normal force measurements, but it is
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