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Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise (1939)
NASA Technical Reports Server (NTRS) · leaf 22
I.A.G.A. technical Vote Mo. 716 Fig.9 2 133 4 5 6 7 8 9 Speed coefficient, Cy Figure 9.* Iffeot of angle of dead rlae on oharaoteriatioo at zero trlaaing aoaent.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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