Hydrodynamic Tests of Models of Seaplane Floats (1935)
NASA Technical Reports Server (NTRS) · leaf 21
at etep L/l « 7.91 H/L - 0.111 U/L - 0.833 d/Z i Distanoe of e.g. aft of P.P. Distance of o.g. above bass line feight of model (to scale) Reserve buoyancy Height of thrust line above base line U-l/U * 0.0534 T/I * 1.645 PT » weight of full size a = angls of tangent at water line forward 6X = angle…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
