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Scale Effect of Model in Seaplane-float Investigations (1933)
NASA Technical Reports Server (NTRS) · leaf 21
Figure ll.-X=12, a=6°, v= 2.75 m/s (9.02 ft./sec.) corresponding to V= 9.5 m/s (31.17 ft./sec.)NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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