Tank tests of a model of a flying-boat hull with a fluted bottom (1935)
NASA Technical Reports Server (NTRS) · leaf 11
* > Model 19, Flutes on forebody and afterbody, tail heel angle, 11° 4fi' o I'odel 19-3 Jlutes on forobody only, tail ieel, 15° 30'.angle. Model 19-C Ko flutes, tail keel angle, 15° 301 Lodel 9 J?$ -8 t-3 … Speed, f.p.B. Figure 6.- Effect of flutee on £/H C51
NASA Technical Reports Server (NTRS)
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