.
Troposphere
Stratosphere
Mesosphere
Drops
Pitch up
Remains same
Elevator
Rudder
Aileron
1013mb
101.3 KN/m2
Both a and b
Air specific range
Specific fuel consumption
None
Wing
Fuselage
Hull
Lift is greater than weight
Lift is less than weight
Lift is equal to weight
Angle of attack
Angle of bank
Longitudinal Dihedral angle
Against the wind
Along with wind
None of the above
Low
Good
Excellent
Is applicable to supersonic aircraft
Is applicable to continuous flow
Both a and b
Magnitude of force applied
Length from the C.G
Both a and b
Lateral stability
Longitudinal stability
Dead-beat stability
More
Less
Same
Newton’s 1st law
Newton’s 1st & 2nd law
Newton’s 1st , 2nd & 3nd law
Supersonic -turbojet engine
Subsonic –aircrafts
None of the above
Altimeter
Anemometer
Barometer
Mesosphere
Thermosphere
Troposphere
The aerofoil produces maximum lift
The aerofoil produces zero lift
The highest lift/drag ratio is produced
Temperature
Density
Pressure