Aerospace Engineering > GATE 2020 > Aircraft Performance
A single engine, propeller driven, general aviation airplane is flying in cruise at sea-level condition (density of air at sea-level is 1.225 kg/m³) with speed to cover maximum range. For drag coefficient CD=0.025+0.049CL² and wing loading W/S=9844 N/m², the speed of the airplane is _______ m/s (round off to one decimal place).
Correct : 149.0 to 151.0
Similar Questions
Which one of the following figures represents the drag polar of a general aviation aircraft?
Which of the following statements about a general aviation aircraft, while operating at point Q in the V-n diagram, is/are true?
An airplane experiences a net vertical ground reaction of 15000 N during landing. The weight of the airplane is 10000 N. The landing vertical load factor, defin...
Total Unique Visitors
Loading......