Inside Out Library · Explore

Calculated effect of various types of flap on take-off over obstacles (1936)

NASA Technical Reports Server (NTRS) · leaf 23

An illustration from Calculated effect of various types of flap on take-off over obstacles, 1936, leaf 23
figure 8.-Variation of total take-off distance at best flap angle with power loading.(Wing loading, W/s = 29.4)

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

More pictures from Calculated effect of various types of flap on take-off over obstacles

More like this