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The Power of Aircraft Engines at Altitude (1939)
NASA Technical Reports Server (NTRS) · leaf 38
Fig. 14.15,20,21,22 N.A.C.A. Technical Memorandum No. 895 1,10 1JO Figure 14.- Variation of O 1,08 power correction factor against O W mixture temper- /,0V a ature. o u u °1,02 1,02 o u wo u © 1,00 o 5 Figure 15.- o 0,98 ^ 0,98 Variation of power correction S G&6 factor versus 4& to inlet tempera-… … 150 200 250 km//? 350 200 250 Mm/Jt 350 mm 600tfgf660/P) mm S0O/tg(SOO/P) and constant Velocity of cooling air speed. Figure 20.- Temperature T variations 250 of the rear spark plug am at constant output at different heights and different wind velocities. mm70Mff(S22fP) ISO Figure 22.- Temperature…NASA Technical Reports Server (NTRS)
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