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Theory of the Landing Impact of Seaplanes (1930)

NASA Technical Reports Server (NTRS) · leaf 41

An illustration from Theory of the Landing Impact of Seaplanes, 1930, leaf 41
HI Figs.12,13,14 N.A.C.A. Technical Memorandum ITo.580 … 180° 170° 160° 150° 140°130° 120° h I Bottom angle Fig. 12 Water pressures at the step of t^rin-float seaplanes of the Heinkel monoplane type. (pn = f [oc fV] theoretically). The pressures are independent of the increases In size of the seaplanes. 10, , sV-V-j H V V-Aiccorditng to V x—i S 6 o d /…

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