Reduction of observed airplane performance to standard conditions (1929)
NASA Technical Reports Server (NTRS) · leaf 8
e of attack or lift coeflB.cient as shown by the slight variation in the ratio which shows a tendency to decrease slowly with in- creasing temperature. The maximmn change in FJFs likely to be encountered in practice is too small to be considered as a correction. A constant lift coefficient or angle… … no no 70 90 50 ■'50 70 90 True airspeed, V,M.P.H. True airspeed, V,M.RH. Fig. 5.—Power curves at 10,00Q-foot pressure altitude. Gross Fig. 4.—Power curves at 10,000-foot pressure altitude. Gross weigbt equals 2,230 pounds. See Figure 4, VE-7 airplane n-eight eqaals 2,230 pounds. See Figure 5, VE-T…
NASA Technical Reports Server (NTRS)
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