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Aviation History
1919
1919 - 1507.PDF
ffi^ NOVEMBER 20, 1919 PRELIMINARY REPORT ON RESISTANCE DUE TO NOSE RADIATOR* THE present report considers the effect of placing a effect of placing a radiator of the same core construc- radiator in the nose of a fuselage as compared with the tion, having an equivalent cooling capacity, in the „ „ , . .. . ,, free air, and streamlining the nose of the fuselage. * From experiments carried out by the Amencan Bureau ™ ,, , ,, ° ,. . ,_„„ Aitt^*.***. of standards, which corresponds to our National Physical The results of these tests indicate less difference Laboratory. than would be shown by comparing results with BUREAU Of STANDARDS AERONAUTIC POWER PLANTS REPORT No. £4-. '-'--23SE fiiSUSCS i£ mSi, ESiiP•' -& t«oe«i--riih-fe»r±mia eiljiifliira Free Air Speed - mi./hr. (V) Plot 1 BUREAU OF STANDARDS . AERONAUTIC POWER PLANTS. REPORT No. 84- . «Ot3. Free Air Speed - Bl./nr. (T) Plot 3 BUREAU OF STANDARDS . AERONAUTIC PQWER PLANTS . HE PORT No 84 . Kan Plow of Air - Ibs./eec./.q.ft. front. Plot 2 BUREAU OF .STANDARDS . AERONAUTIC POWER PLANTS REPORT No. fc* Flow of Air - lbs./eec./eq.rt. front. Plot 4 I509
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