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Landing impact of seaplanes (1931)

NASA Technical Reports Server (NTRS) · leaf 32

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1.5 o Test points 1.0 2, 2 at a d M^8 Pm> Cl-0.425 —g) .5 p =Density of vater. d = bj Length of plate edges. 0 12 3 4 Aspect ratio Fig. 2 The accelerated wrter mass of rectangular plates in a one—sided floi». ,0 xi rni. Fig. 3 Systems consisting of seaplane and water mass.

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