Static stability - Flight Mechanics & Space Dynamics - Aerospace Engineering Previous Year Questions

For maximum range of a glider, which of the following conditions is true?

An airplane with a larger wing as compared to a smaller wing will necessarily have

Two airplanes are identical except for the location of the wing. The longitudinal static stability of the airplane with low wing configuration will be

For a fixed center of gravity location of an airplane, when the propeller is mounted on the nose of the fuselage

If horizontal tail area is increased while the elevator to horizontal tail area ratio is kept same, then

If during the maximum rate of climb at 5 km altitude, the airplane was flying at an angle of attack of 4 degrees and attitude (pitch) angle of 5 degrees, what was equivalent airspeed of the airplane?

An aircraft has a level flight stalling speed of 60 m/s EAS (equivalent air speed). As per the V-n diagram, what is the minimum speed at which it should be designed to withstand the maximum vertical load factor of 9?

The primary function of the fin in the vertical tail of an aircraft is to provide

An aircraft requires the trailing edge of the elevator to be deflected upwards from its initial position to lower the trim speed. Which of the following statements about the static stick-fixed stability of this aircraft is true?