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Gyroscope (mechanism) is used to determine the effect of a turn taken by an aeroplane. In a short let me describe them,

1. If the rotation of a propeller/ rotor is in CLOCKWISE when viewed from REAR/ BACK SIDE and the aeroplane takes a LEFT TURN, then reactive gyroscopic couple (which is equal in magnitude and opposite in direction of active gyroscopic couple) will tend to RAISE THE NOSE and DIP THE TAIL.

2. If the above similar conditions are considered when the plane is taking a RIGHT TURN, then the reactive gyroscopic couple will tend to RAISE THE TAIL & DIP THE NOSE.

3. If the rotation of a propeller is in ANTI-CLOCKWISE DIRECTION when viewed from REAR of the aeroplane and the plane takes a LEFT TURN, the reactive gyroscopic couple tend to RAISE THE TAIL & DIP THE NOSE.

4. If we consider the similar conditions of (3), and a plane takes a RIGHT TURN, then the reactive gyroscopic couple tends to RAISE THE NOSE & DIP THE TAIL.

To remember it easily, you can use RIGHT HAND SCREW RULE.

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Q: What is Gyroscopic effect on aeroplane?
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How gyroscopic couple work in a aroplanes and ship?

Effect of the Gyroscopic Couple on an ship and Aeroplane :-Ships and aeroplanes consist of large moment of inertia propeller and fly wheels. When aeroplane or ship takes right or left turn there occurs a rate of change of angular momentum because of change of direction of angular momentum vector. Thus a counter couple is produced when they terns.When the engine or propeller of aeroplane or fly wheel of ship rotate such that the spin angular momentum vector is along the sailing direction and when the aeroplane or ship takes a left turn, then the effect of reactive gyroscopic couple will be to dip the nose (stem: for ship) and raise the tail of the aeroplane or ship.When the aeroplane or ship takes a right turn under similar conditions above, the effect of reactive gyroscopic couple will be to raise the nose and dip the tail of the aeroplane or ship.In the case of ships the fly wheel must be mounded such that the spin axis is along the length so as to maintain dynamic stability.


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