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Experiments with a built-in or fuselage radiator (1923)
NASA Technical Reports Server (NTRS) · leaf 15
160 14-0 o 120 o 100 CD SO o ll 6o H-o 20 0 20 30 ^0 50 10 Vrm/sec Fig- 3 Quantity of air flowing tnrough radiator plotted against speed Q=cu,£ %} sec … Q=l/sec a=20 m/sec (65*6 ft/sec) b=30 m/sec (9&A ft/sec) c=40 m/sec (I3I.2 ft/sec) d=50 m/sec (164--0 ft/sec) Fig. *f Resistance Surface plotted against airflow at different speedsNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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