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- gyroscopic instruments - Gyro Erection System - Aviation Stack Exchange
I have a hard time understanding the physics behind the pneumatic erecting system in an attitude indicator According to my book and the linked image, the applied force is “precessed 90 degrees” (a
- Is precession a problem for two-bladed propellers?
0 Precession is a gyroscopic effect, and –for the same angular speed– the forces involved depend on the moment of inertia of the propeller, that (for the same blade configuration and materials) is proportional to the number of blades
- Engine torque due to Turbofan engines and its effect on aircraft . . .
I know that for turbofan engines there will be Gyroscopic effects while pitching, rolling and yawing maneuvre But if the aircraft is cruising at an altitude or is simply idling on the ground, what
- aircraft design - Do gyroscopic forces (from rotating engines . . .
Gyroscopic forces are a factor on propellor driven aircraft, but generally not noticeable on a stable ('God Fearing') aircraft in cruise flight However gyroscopic effects do become noticeable in several areas of a propellor driven aircraft's flight envelope One of the best known areas are in dramatic changes in pitch attitude at low speeds
- military - How did the gyro gunsights of WW2 get the range and lead of . . .
I just read this article on the gyro gunsight, but I don't understand how it computed range position to the target and then calculated how much lead is needed Surely it must have had radar to get
- aerodynamics - If the RPM of the Gyro is increased due to high Vacuum . . .
When the rotor is made to spin, the device becomes a gyroscope possessing two properties : Rigidity (or gyroscopic inertia); and Precession Rigidity Rigidity is the property of a gyroscope which resists any force tending to change the plane of rotation of its rotor As a result of rigidity, the spin axis tends to maintain a fixed direction in
- flight instruments - Why is the turn coordinator gyro tilted . . .
The turn coordinator is a rate gyro Unlike attitude and heading gyros that are free to rotate and the instrument senses the orientation of their axis, the turn coordinator (and the turn indicator one) has the axis mounted fixed and the instrument measures the torque forces as the gyroscope tries to resist the rotational motion With the axis mounted along the longitudinal axis in a turn rate
- Use of Gyroscopes in instruments - Aviation Stack Exchange
After arguing with ChatGPT and trying to find explanations of gyroscopes on the internet for days, I'm finally turning to ASE in hopes for an explanation about Gyroscopic instruments Some backgro
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