Inside Out Library · Explore

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 26

An illustration from 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, leaf 26 — -4 -3 0 3 4 6 8 Trim, deg. Figure 13.- Effect of angle of dead riBe and extended bow on static properties. Initial load coefficient 0A « 1.575.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

More pictures from 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

More like this