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Development of the Rules Governing the Strength of Airplanes. Part I : German Loading Conditions up to 1926 (1933)
NASA Technical Reports Server (NTRS) · leaf 60
Jigs. 2,7,14.15 N.A.C.A. Technical Memorandum No. 716 … Figure 7*-Ca'ble tensometer (taken - from B & A of the WSL 1922, p.148, fig.25). Oil inlet ♦To indi- cator Figure 15#-Deflections of leading edge of wing (so-urce Z5M, 1916, p.29, fig. 12) • — Figare 14.-Sketc]a of wing with load cliart (soxircet ZIM, 1916, p.29, fig.9).NASA Technical Reports Server (NTRS)
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