Reduction of observed airplane performance to standard conditions (1929)
NASA Technical Reports Server (NTRS) · leaf 12
367 REDUCTION OF AmPI^ANE PERFORMANCE TO STANDARD CONDITIONS … True air speed, V,M.P.H. Trus airspeed. V,M.P.H. Fio. 17.—Power curves at 10,000-foot pressure altitude with temper- Fig. 16.—Power carves at 10,000-foot pressure altitude with tem- atures 120 per cent normal. Kormal piraiite. r=l.20 r. perature 83.3 per cent normal. Stanvil paraaiU. 2'=o.833 T,
NASA Technical Reports Server (NTRS)
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