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The 1926 German seaplane contest (1928)
NASA Technical Reports Server (NTRS) · leaf 33
N.A.C.A. Technical Memorandum No,454 500 450 400 km/h 350 300 250 200 t •2( hi! 150 0^=18ad load(kg) 100 G_ =ratabl8 use- 2w ful load(kg) 50 S=flight range (km) 0 t=climbing time 400 400 … .3 .4 .5 .6 .7 .8 .9 1.0 Fig.2 Relation between dead load,flight rang* climbing time and horizontal speed of ' seaplane,NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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