[CLO-1] For small propeller airplanes with the given information estimate the maximum Rang and max endurance.\
c=3x10$^{-7}$ (1/\(\rho\)), S=160 ft$^2$, AR=7, total weight=3000 lb, fuel weight =300 lb, $\eta_{propeller}$=0.85, at see level where density is 0.002377 slug/ft$^3$, g=32.2 ft/s$^2$ and Thrust T=706.6 lb, form the performance curve we have (CL)$_{max}$=1, (CL/CD)$_{max}$=12.5 and (CL$^{3/2}$/CD)$_{max}$=12 ?\
Rmax=6376975 ft, Emax=51922 sec\
None of the anwers\
Rmax=1207 mile, Emax=14.4 hr\
Rmax=706.7 mile, Emax=7.87 hr