Maximum amount of transverse righting moment at rest provided by auxiliary floats or stub wings compared with minimum righting moment required by certain specifications: adequacy of stability evaluated in terms of pilots' opinions based on which U S Navy specification for seaplanes apparently will provide wing tip float having adequate displacement.
Comparison of design specifications with actual static transverse stability of 25 seaplanes
National Advisory Committee Aeronautics -- Technical Note
1947
12 pages
8 Supplementary Plates
Report
Englisch
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