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Charts for calculating the performance of airplanes having constant-speed propellers (1936)
NASA Technical Reports Server (NTRS) · leaf 15
.7 .8 1.0 .6 .5 Figure 3,- Tariation of thrust horsepower with velocity at constant, engine speed, t. hp. at ■ T t. hp.,at \= 1.0NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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