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Performance of Maybach 300-horsepower airplane engine (1923)

NASA Technical Reports Server (NTRS) · leaf 7

An illustration from Performance of Maybach 300-horsepower airplane engine, 1923, leaf 7
96 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. … LOO .80 .$ -GO " *.40 .20 /Vole:- The carburetor air temperature was held at 59*6'during fheMoybach J_ O tests but in testing the other engines \ was changed at each dens/fys its value ~ being 59 fCat the highest density ona WE ot the lowest density .070 .060 .050 .040 .030 .060 .050 .040 Fig. II…

NASA Technical Reports Server (NTRS)

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