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Hydrodynamic tests for determining the take-off characteristics of seaplanes (1923)
NASA Technical Reports Server (NTRS) · leaf 13
6393 -992 v m 11332 13801 ^610 "i6^123!7l *7.* Wi 82.0 ffit 115-v i» -—— - ~ - ~ . -i 3000 35 Vi'n m/ssc. 15 20 25 . 30 64-00 6260 5g4-o 5i4o 4-i60 2900 1360 450 W in kg. Fig>3- 13871 H975 2502 W in 1J?;. 14110 13162 . 107*9 „ „ 0 16.4- 32.S U9.2 co'.tS7 82.0 115 131 V in ft/sec … 15 20 25 30 35 *0 v in m/ss©, 0 5 10 5^32 4S80 3712 2530 II35 W in kg. 64-00 6290 5970 Fx CT - Hydro dynamic resistance in kg. of two full-sis e floats coupled.together with an intervening space of 5m(16,4ft) at progressive speeds and for given longitudinal trims by computing the lifting., effect…NASA Technical Reports Server (NTRS)
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