A jet airplane has the Ta−Tr curves shown in Figure 6.17. The airplane data are gross weight = 10 000 lb, standard sea level day, rpm at 100% unless noted, and clean configuration. Find:

a. Vmax at 95% rpm.

b. V for maximum climb angle.

c. Maximum climb angle.

d. Rate of climb at 400 kts.

e. V for best endurance.

f. V for maximum range.
g. V for maximum range with 100 kts. of headwind.