Hydrodynamic and Aerodynamic Tests of a Family of Models of Seaplane Floats with Varying Angles of Dead Rise - N.A.C.A. Models 57-A, 57-B, and 57-C (1939)
NASA Technical Reports Server (NTRS) · leaf 23
A.C.A. Teonnical Not* Ho 716 Tig.10 8peed coefficient, Oy Figure 10.- Effect of angle of dead rise on characterietioe at beet trim.
NASA Technical Reports Server (NTRS)
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