Hydrodynamic Tests of Models of Seaplane Floats (1935)
NASA Technical Reports Server (NTRS) · leaf 23
. aft of 7.P. Z - 387.5 mm Distance of o.g. above base line 179 mm Weight of model (to soale) P = 1.333 kg Reserve buoyancy Vt - 0.993 kg Height of thrust line above base line Tn = 179 mm M-I/K - 0.0650 Y/H -3.430 PT ■ weight of full sire a = angle of tangent at water line forward 6i = angle…
NASA Technical Reports Server (NTRS)
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